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~CFGET

 

~CFGET, Par, Entity, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

Obtains values from the CivilFEM database and stores them in a user defined parameter

DATABASE: Parameter

Par

The name of the resulting parameter.

Entity

Entity keyword. Valid keywords are shown in the table below.

ACTIVE

CivilFEM general data

MATERIAL

Material properties

SECTION

Cross sections properties

SHLVERT

Shell vertices properties

MEMBPROP

Code member properties

BMSHPROP

Beam or shell properties

SLDSEC

Solid sections properties

ELEMENT

Solution at element and section level

SOLID

Solution at solid section level

SLOPE

Properties related to slope stability

FOUNDAT

Properties related to foundation

TERRAIN

Properties related to terrain

WALL

Properties related to retaining walls

BRIDGE

Properties related to the bridges module

PRSCONC

Properties related to the prestressed module

FRAME

Properties related to predesigned frames

SEISM

Properties related to seismic analysis

 

ENTNUM

Entity number. Valid values are the ones described in the tables below.

Lab1

Name of a particular item for the given entity. Valid values for each entity are the ones described in the columns of the following tables referred to Lab1.

Lab2, Lab3

Additional sets of item labels to further qualify the item for which data are to be retrieved. Valid values for each Lab1 are described in the following tables. Most parameters do not need a value of Lab3.

IDX1, IDX2, IDX3

Numbers identifying the data defined in Lab1, Lab2 and Lab3. Most data do not need that level of information.

Most of the parameters are stored in the CivilFEM database and can be recovered at any given moment. The different properties are grouped according to the entities to which they belong (ENTNUM) in the following order:

 

·         ~CFGET - CONFIG

·         ~CFGET - ACTIVE

·         ~CFGET - MATERIAL

·         ~CFGET - SECTION

·         ~CFGET - SHLVERT

·         ~CFGET - MEMBPROP

·         ~CFGET - BMSHPROP

·         ~CFGET - SLDSEC

·         ~CFGET - ELEMENT

·         ~CFGET - SOLID

·         ~CFGET - SLOPE

·         ~CFGET - FOUNDAT

·         ~CFGET - TERRAIN

·         ~CFGET - WALL

·         ~CFGET - BRIDGE

·         ~CFGET - PRSCONC

·         ~CFGET - FRAME

·         ~CFGET - SEISM

 

·         ~CFGET – CONFIG (ENTNUM = 0 or blank)

 

~CFGET, Par, CONFIG, 0, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= AS3600

~CFGET, Par, CONFIG, 0, AS3600, Lab2, , IDX1, IDX2, IDX3

Retrieves configuration data for the Australian AS3600 code. Valid labels are:

Lab2

Description

PHI

Strength reduction factor for axial+bending.

 

Lab1= SP52101

~CFGET, Par, CONFIG, 0, SP52101, Lab2, , IDX1, IDX2, IDX3

Retrieves configuration data for the Russian SP 52-101 code. Valid labels are:

Lab2

Description

PHIB1

Strength reduction factor.

 

Lab1= SP63133

~CFGET, Par, CONFIG, 0, SP63133, Lab2, , IDX1, IDX2, IDX3

Retrieves configuration data for the Russian SP 63.13330.2012 code. Valid labels are:

Lab2

Description

PHIB1

Strength reduction factor.

 

Lab1= DINTER

~CFGET, Par, CONFIG, 0, DINTER, Lab2, , IDX1, IDX2, IDX3

Retrieves configuration data for interaction diagram. Valid labels are:

Lab2

Description

NED

Number of steps on strains.

NTD

Number of steps on angles.

N2D

Number of steps on 2D analysis.

WMIN

Minimum reinforcement factor.

WMAX

Maximum reinforcement factor.

DELTA

Diagram center coefficient.

LIMCOUNT

Maximum number of iterations on design.

NMAXDIAG

Maximimum number of diagrams sotred in file.

 

Lab1= RCV

~CFGET, Par, CONFIG, 0, RCV, Lab2, , IDX1, IDX2, IDX3

Retrieves configuration data for results file (*.RCV). Valid labels are:

Lab2

Description

RESMAX

Maximum number of records in CivilFEM results file.

 

·         ~CFGET – ACTIVE (ENTNUM = 0 or blank)

 

~CFGET, Par, ACTIVE, 0, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= MATERIAL

~CFGET, Par, ACTIVE, 0, MATERIAL, Lab2, , IDX1, IDX2, IDX3

Retrieves data of materials. Valid labels are:

Lab2

Description

COUNT

Total number of defined materials.

MAX

Maximum number assigned to existing materials

MIN

Minimum number assigned to existing materials.

 

Lab1= CROSSEC

~CFGET, Par, ACTIVE, 0, CROSSEC, Lab2, , IDX1, IDX2, IDX3

Retrieves data of cross sections. Valid labels are:

Lab2

Description

COUNT

Total number of defined cross sections.

MAX

Maximum number assigned to existing cross sections.

MIN

Minimum number assigned to existing cross sections.

 

Lab1= SHLVERT

~CFGET, Par, ACTIVE, 0, SHLVERT, Lab2, , IDX1, IDX2, IDX3

Retrieves data of shell vertices. Valid labels are:

Lab2

Description

COUNT

Total number of defined shell vertices.

MAX

Maximum number assigned to existing shell vertices.

MIN

Minimum number assigned to existing shell vertices.

 

Lab1= MEMBPROP

~CFGET, Par, ACTIVE, 0, MEMBPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties data. Valid labels are:

Lab2

Description

COUNT

Total number of defined member properties.

MAX

Maximum number assigned to existing member properties.

MIN

Minimum number assigned to existing member properties.

 

Lab1= BMSHPROP

~CFGET, Par, ACTIVE, 0, BMSHPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to beam and shell properties. Valid labels are:

Lab2

Description

COUNT

Total number of defined beam and shell properties.

MAX

Maximum number assigned to existing beam and shell properties.

MIN

Minimum number assigned to existing beam and shell properties.

 

Lab1= SLDSEC

~CFGET, Par, ACTIVE, 0, SLDSEC, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to solid sections properties. Valid labels are:

Lab2

Description

COUNT

Total number of defined solid sections.

MAX

Maximum number assigned to existing solid sections.

MIN

Minimum number assigned to existing solid sections.

 

Lab1= CODE

~CFGET, Par, ACTIVE, 0, CODE, Lab2, , IDX1, IDX2, IDX3

Retrieves active codes. Valid labels are:

Lab2

Description

STEEL

Structural steel active code.

CONCR

Concrete active code.

PREST

Prestressed concrete active code.

SEISMIC

Seismic active code.

 

Lab1= ACTTIME

~CFGET, Par, ACTIVE, 0, ACTTIME, , , IDX1, IDX2, IDX3

Retrieves active time (in days).

 

Lab1= UNITS

~CFGET, Par, ACTIVE, 0, UNITS, Lab2, Lab3, IDX1, IDX2, IDX3

Retrieves active units (conversion factors to convert from the active system to the International System and labels). Valid labels are:

Lab2

Lab3

Description

LENG

VALUE

Conversion factor for the length unit.

LENG

NAME

Label identifying the length unit.

TIME

VALUE

Conversion factor for time unit.

TIME

NAME

Label identifying the time unit.

FORC

VALUE

Conversion factor for the force unit

FORC

NAME

Label identifying the force unit

MASS

VALUE

Conversion factor for the mass unit.

MASS

NAME

Label identifying the mass unit.

PRES

VALUE

Conversion factor for the pressure unit.

PRES

NAME

Label identifying the pressure unit.

MONE

VALUE

Conversion factor for monetary unit.

MONE

NAME

Label identifying monetary unit.

 

Lab1= TERRAIN

~CFGET, Par, ACTIVE, 0, TERRAIN, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to active soils. Valid labels are:

Lab2

Description

COUNT

Total number of terrains.

MAX

Maximum number of terrains.

MIN

Minimum number of terrains.

 

·         ~CFGET – MATERIAL (ENTNUM = Number of material)

~CFGET, Par, MATERIAL, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= DATGEN

~CFGET, Par, MATERIAL, ENTNUM, DATGEN, Lab2, , IDX1, IDX2, IDX3

Retrieves general data common to all materials. Valid labels are:

Lab2

Description

NAME

Name assigned to the material (32 characters). IDX1 indicates the group of 8 characters to recover.

IDX1

Name

1

1 to 8

2

9 to 16

3

17 to 24

4

25 to 32

Ref8

Reference of the defined material through the library.

TYPE

Type of material.

TACT

Activation time of the material.

TDEACT

Deactivation time of the material.

EX

Modulus of elasticity.

NUXY

Poisson’s ratio.

GXY

Transverse strain modulus.

ALP

Coefficient of thermal expansion.

RHO

Density of the material.

GAM

Specific weight of the material.

DAMP

Damping of the material.

VCOS

Cost of the material per unit volume.

MCOS

Cost per mass unit.

WCOS

Cost per weight unit.

 

Lab1= STEEL

~CFGET, Par, MATERIAL, ENTNUM, STEEL, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of structural steel material. Valid labels are:

Lab2

Description

NTHK

Number of ranges of thickness.

THIK

Thickness corresponding to the different existing ranges. In IDX1 the corresponding range of thickness must be indicated.

EXLN

Modulus of elasticity for linear analysis.

KPLA

Behavior of the material: 0- Elastic, 1- Bilinear kinematic, 2- Bilinear isotropic, 3- Multilinear elastic, 4- Multilinear kinematic, 5- Multilinear isotropic, 6- Drucker Prager

PLRAT

Ratio between the modulus of elasticity and the plastic modulus.

PLThk

Thickness used to defined the plastic behavior.

TSASSD

Type of stress-strain diagram for structural analysis:

0- User defined, 1- Elastic-linear, 2- Bi-linear.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis.

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the range of thickness indicated in IDX2.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the range of thickness indicated in IDX2.

TSDSSD

Type of the stress-strain diagram for analysis of sections: 0- User defined, 1- Bi-linear with horizontal top branch, 2- Bi-linear with inclined top branch.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the range of thickness indicated in IDX2.

SDSGM

Stress value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the range of thickness indicated in IDX2.

EPSMAX

Maximum valid tension strain.

EPSMIN

Maximum valid compression strain.

STYPE

Steel type: 0- Non austenitic, 1- Austenitic.

 

Lab1= CONCR

~CFGET, Par, MATERIAL, ENTNUM, CONCR, Lab2, , IDX1, IDX2, IDX3

Retrieves the specified data of the concrete material. Valid labels are:

Lab2

Description

NAGE

Number of age points defined for the material.

AGE

Age value for the point specified in IDX1.

MATAGE

Age of the material.

TPEX

Type of elasticity modulus defined:

1

Tangent modulus.

2

Initial modulus.

3

Secant modulus.

4

Design modulus of elasticity.

5

Reduced modulus of elasticity.

EXLN

Modulus of elasticity for linear analysis.

EPSMIN

Maximum valid compression strain.

EPSINT

Maximum valid compression strain in internal points of the section.

PCLEVEL

Distance from the most compressed fiber of the section to the interior compression rupture pivot (point C).

KCREEP

Creep method.

0

No creep.

1

Step by step.

2

Effective Modulus

KSHRINK

Shrinkage method.

0

No shrinkage.

1

By temperatures.

AGECOEF

Aging coefficient.

AGESRINI

Shrinkage initial age in concrete

TAPPLOAD

Load aplication time

NAPT

Number of load application ages defined.

APT

Load application age defined in IDX1.

CREEPCF

Creep coefficient at point IDX1, IDX2:

IDX1

Age index.

IDX2

Load application age index.

EPSSHRNK

Shrinkage strain for age index IDX1.

KCRCOD

Calculation method for the shrinkage strains and creep coefficients curves.

0

User defined

1

EC2 Model

2

CEB Model

3

ACI Model

4

EHE Model

RH

Relative humidity (%). Valid for the curves calculation using EC2, CEB and EHE models.

H

Fictitious thickness in milimeters. Valid for the curves calculation using EC2, CEB and EHE models.

PSI

Creep factor. Valid for the curves calculation using ACI model.

D

Creep age (days). Valid for the curves calculation using ACI model.

NUU

Ultimate (in time) creep coefficient. Valid for the curves calculation using ACI model.

ALPHA

Shrinkage factor. Valid for the curves calculation using ACI model.

F

Shrinkage age. Valid for the curves calculation using ACI model.

EPSSLU

Ultimate (in time) shrinkage strain. Valid for the curves calculation using ACI model.

 

Lab1= REINF

~CFGET, Par, MATERIAL, ENTNUM, REINF, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of the steel reinforcement material. Valid labels are:

Lab2

Description

EPSMAX

Maximum strain valid in tension.

 

Lab1= PREST

~CFGET, Par, MATERIAL, ENTNUM, PREST, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of the prestressed steel material. Valid labels are:

Lab2

Description

EPSMAX

Maximum permissible tension strain

MU

Tendon sheath friction coefficient

K

Parasitic friction coefficient per length unit

A

Anchorage slip

EPSSR

Concrete shrinkage strain

PHI

Concrete creep coefficient

 

Lab1= EC3

~CFGET, Par, MATERIAL, ENTNUM, EC3, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Eurocode 3. Valid labels are:

Lab2

Description

GAMM0

Partial safety factor of class 1, 2 or 3 sections resistance.

GAMM1

Partial safety factor of the class 4 sections resistance.

GAMM2

Partial safety factor of net sections resistance.

FY

Steel’s elastic limit for the thickness range specified in IDX1.

FU

Steel ultimate strength load for the thickness range specified in IDX1.

 

Lab1= CTESEA

~CFGET, Par, MATERIAL, ENTNUM, CTESEA, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of CTE DB SE-A code. Valid labels are:

Lab2

Description

GAMM0

Partial safety factor of class 1, 2 or 3 sections resistance.

GAMM1

Partial safety factor of the class 4 sections resistance.

GAMM2

Partial safety factor of net sections resistance.

FY

Steel’s elastic limit for the thickness range specified in IDX1.

FU

Steel ultimate strength load for the thickness range specified in IDX1.

 

Lab1= EA

~CFGET, Par, MATERIAL, ENTNUM, EA, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of EA code. Valid labels are:

Lab2

Description

GAMA

Reduction coefficient.

SIGE

Steel’s elastic limit for the thickness range indicated in IDX1.

SIGR

Calculation resistance of steel (SIGE/GAMA) for the thickness range indicated in IDX1.

SIGU

Maximum tension resistance of steel for thickness range indicated in IDX1.

 

Lab1= BS595085

~CFGET, Par, MATERIAL, ENTNUM, BS595085, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of BS5950085 or BS595001. Valid labels are:

Lab2

Description

YS

Steel’s elastic limit for the thickness range indicated in IDX1.

US

Tension resistance of steel for thickness range indicated in IDX1.

ROY

Design strength of steel for the thickness range indicated in IDX1.

KE

Effective area/net area ratio for the thickness range indicated in IDX1.

 

Lab1= LRFD

~CFGET, Par, MATERIAL, ENTNUM, LRFD, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of AISC-LRFD second edition. Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= LRFD13

~CFGET, Par, MATERIAL, ENTNUM, LRFD13, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of AISC-LRFD 13th edition. Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= GB50017

~CFGET, Par, MATERIAL, ENTNUM, GB50017, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of GB50017 code. Valid labels are:

Lab2

Description

F

Tensile, compressive or bending strength.

FCE

Compression strength when ending section is under compression

FV

Shear strength.

 

Lab1= AASHTO10

~CFGET, Par, MATERIAL, ENTNUM, AASHTO10, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of AASHTO LRFD BRIDGE DESIGN SPECIFICATIONS (2010). Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= IS800-07

~CFGET, Par, MATERIAL, ENTNUM, IS800-07, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Indian Standard 800 (2007). Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= ASME_NF

~CFGET, Par, MATERIAL, ENTNUM, ASME_NF, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of ASME BPVC III Subsection NF. Valid labels are:

Lab2

Description

SY

Elastic limit of steel for range of thickness specified in IDX1.

SU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= ASD9

~CFGET, Par, MATERIAL, ENTNUM, ASD9, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of AISC-ASD Ninth Edition. Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= ASD13

~CFGET, Par, MATERIAL, ENTNUM, ASD13, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of AISC 13th Edition. Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= AISC14

~CFGET, Par, MATERIAL, ENTNUM, AISC14 Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of AISC 14th Edition. Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= AISC15

~CFGET, Par, MATERIAL, ENTNUM, AISC15 Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of AISC 15th Edition. Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= N690

~CFGET, Par, MATERIAL, ENTNUM, N690, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of ANSI/AISC N690 code. Valid labels are:

Lab2

Description

FY

Elastic limit of steel for range of thickness specified in IDX1.

FU

Ultimate strength of steel for range of thickness specified in IDX1.

 

Lab1= EC2_C

~CFGET, Par, MATERIAL, ENTNUM, EC2_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data referring to Eurocode 2 concrete material. Valid labels are:

Lab2

Description

CETP

Type of cement.

S

Slow hardening cements

N

Normal hardening cements

R

Rapid hardening cements

RS

Rapid hardening-high strength cements

GAMC

Partial safety factor for concrete.

ALP

Additional reduction factor for sustained compression.

FCK

Characteristic 28-day compressive strength.

FCM

Mean 28-day compressive strength.

FCD

Design 28-day compressive strength.

FCTM

Mean tensile strength.

FCTK_005

Lower characteristic tensile strength.

FCTK_095

Upper characteristic tensile strength.

EPSC1

Strain of the concrete’s peak compressive stress.

EPSCU

Compression ultimate strain.

S

Coefficient which depends on the type of cement.

BETCC

Coefficient which depends on concrete age for the age index specified in IDX1.

FCM_T

Mean t day compressive strength corresponding to the age index indicated in IDX1.

FCK_T

Characteristic compressive strength corresponding to the age ratio indicated in IDX1.

FCD_T

Design compressive strength corresponding to the age ratio indicated in IDX1.

ECM

Secant modulus of elasticity corresponding to the age ratio indicated in IDX1.

EC

Tangent modulus of elasticity corresponding to the age ratio indicated in IDX1.

ECD

Design modulus of elasticity corresponding to the age ratio indicated in IDX1.

TSASSD

Type of stress-strain diagram for structural analysis:

 0- User defined, 1- Elastic-linear, 2- Short term loads.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the age index indicated in IDX2.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the age index indicated in IDX2

TSDSSD

Type of the stress-strain diagram for analysis of sections: 0- User defined, 1-Parabolic-rectangular, 2- Bi-linear.

NPSDSSD

Number of points of the stress-strain diagram of the analysis of sections.

SDEPS

Strain value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the age index indicated in IDX2.

SDSGM

Stress value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the age index indicated in IDX2.

 

Lab1= EC2_S

~CFGET, Par, MATERIAL, ENTNUM, EC2_S, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Eurocode 2 referred to reinforcement steel material. Valid labels are:

Lab2

Description

GAMS

Steel’s safety factor.

FYK

Characteristic yield stress.

FYD

Design yield stress.

FTK

Characteristic tensile strength.

EPSUK

Characteristic elongation at maximum load.

DUCT

Steel ductility (character parameter):

HIGH

NORMAL

NONE

TSASSD

Type of stress-strain diagram of structural analysis:

0- User defined, 1- Elastic-linear, 2- Bi-linear.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis.

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

TSDSSD

Type of strain-stress diagram for analysis of sections:
0- User defined,
1- Bi-linear with horizontal top branch,
2- Bi-linear with inclined top branch.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point of the analysis stress-strain diagram specified in IDX1.

 

Lab1= EC2_PRE

~CFGET, Par, MATERIAL, ENTNUM, EC2_PRE, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Eurocode 2 referred to prestressed steel material. Valid labels are:

Lab2

Description

GAMS

Prestessed steel’s safety factor.

FPK

Stress characteristic strength

FPO1K

Characteristic stress value that produces a 0.1% remaining strain.

EPSUk

Characteristic elongation at maximum load

R0-60

Relaxation at 1000 hours and 60% of the fpk

R0-70

Relaxation at 1000 hours and 70% of the fpk

R0-80

Relaxation at 1000 hours and 80% of the fpk

LTRAT

Relation between the breathing long term losses and the corresponding ones to 1000 hours.

TSASSD

Type of stress-strain diagram of structural analysis:

0- User defined, 1- Elastic-linear, 2- Bi-linear

NPSASSD

Number of points of the stress-strain diagram of the structural analysis.

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

TSDSSD

Type of strain-stress diagram for analysis of sections: 0- User defined, 1- Bi-linear with horizontal top branch, 2- Bi-linear with inclined top branch.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point of the analysis stress-strain diagram specified in IDX1.

 

Lab1= ACI_C

~CFGET, Par, MATERIAL, ENTNUM, ACI_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of the ACI code referred to concrete material. Valid labels are:

Lab2

Description

CUTP

Type of curing (parameter of characters):

MOIST

“Moist cured”

STEAM

“Steam cured”

CETP

Type of cement (characters parameter):

I

Type of cement I

III

Type of cement III

FC

Specified compressive strength.

A

Coefficient depending on the type of cement and curing.

BET

Coefficient depending on the type of cement and curing.

FC_T

Compressive strength at any age. The age must be defined in IDX1.

FR

Modulus of rupture. The age must be defined in IDX1.

EC

Modulus of elasticity of concrete corresponding to the age index defined in IDX1.

BET1

Coefficient for rectangular stress distribution. This factor depends on the FC value.

EPS0

Strain corresponding to the peak compressive stress in the parabolic stress-strain diagram for the age index indicated in IDX1.

TSASSD

Type of stress-strain diagram for structural analysis: 0- User defined, 1- Elastic-linear, 2- PCA Parabolic.

NPSASSD

Number of points of the stress-strain diagram of structural analysis.

SAEPS

Value of the strain of a point of the stress-strain diagram of structural analysis specified in DX1 for the age index indicated in IDX2.

SASGM

Value of the stress of a point of the stress-strain diagram of structural analysis specified in DX1 for the age index indicated in IDX2.

TSDSSD

Type of stress-strain diagram for analysis of sections: 0- User defined, 1- PCA Parabolic, 2- Rectangular, 3-Lineal, 4-Parabolic (Default value if the active code is ACI 359).

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Value of strain of the point of the analysis stress-strain diagram specified in IDX1 for the age index indicated in IDX2.

SDSGM

Value of the stress of the point of the analysis stress-strain diagram specified in IDX1 for the age index indicted in IDX2.

 

Lab1= ACI_S

~CFGET, Par, MATERIAL, ENTNUM, ACI_S, Lab2, , IDX1, IDX2, IDX3

Retrieves the specific data of the ACI code referred to the reinforcement steel material. Valid labels are:

Lab2

Description

FY

Specified yield strength.

TSASSD

Type of stress-strain diagram for structural analysis:

0- User defined, 1- Elastic-linear, 2-Bi-linear.

NPSASSD

Number of points of the stress-strain diagram of structural analysis.

SAEPS

Strain value at the point of the stress-strain diagram of structural analysis specified in IDX1.

SASGM

Stress value at the point of the stress-strain diagram of structural analysis specified in IDX1.

TSDSSD

Type of stress-strain diagram for analysis of sections:

 0- User defined, 1- Bi-linear.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value at the point of the analysis stress-strain diagram specified in DX1.

SDSGM

Stress value at the point of the analysis stress-strain diagram specified in DX1.

 

Lab1= ACI_PRES

~CFGET, Par, MATERIAL, ENTNUM, ACI_PRES, Lab2, , IDX1, IDX2, IDX3

Retrieves the specific data of the ACI code referred to the reinforcement steel material. Valid labels are:

Lab2

Description

FPU

Specific tensile strength

FPY

Specific elastic limit

STTP

Steel type: 0- Low relaxation, 1- Stress-relieved.

RLCF1

Relaxation calculation coeffcient

RLCF2

Relaxation calculation coeffcient

TSASSD

Type of stress-strain diagram for structural analysis:

0- User defined, 1- Elastic-linear, 2-Bi-linear.

NPSASSD

Number of points of the stress-strain diagram of structural analysis.

SAEPS

Strain value at the point of the stress-strain diagram of structural analysis specified in IDX1.

SASGM

Stress value at the point of the stress-strain diagram of structural analysis specified in IDX1.

TSDSSD

Type of stress-strain diagram for analysis of sections:

 0- User defined, 1- Bi-linear.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value at the point of the analysis stress-strain diagram specified in DX1.

SDSGM

Stress value at the point of the analysis stress-strain diagram specified in DX1.

 

Lab1= CEB_C

~CFGET, Par, MATERIAL, ENTNUM, CEB_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of model code CEB-FIP referred to concrete material. Valid labels are:

Lab2

Description

CETP

Type of cement (characters parameter):

SL

Slow hardening cements.

N

Normal hardening cements.

R

Rapid hardening cements.

RS

Rapid hardening-high strength cements.

GAMC

Concrete’s safety factor

FCK

Characteristic compressive strength.

FCD

Design compressive strength.

FCM

Mean compressive strength.

FCTK_MIN

Lower characteristic tensile strength.

FCTK_MAX

Upper characteristic tensile strength.

FCTM

Mean tensile strength.

S

Coefficient which depends on the type of cement.

BETCC

Coefficient depending on the concrete’s age for the age index specified in IDX1.

FCM_T

Mean compressive strength of concrete for the age index specified in IDX1.

FCK_T

Characteristic compressive strength of concrete for the age index specified in IDX1.

FCD_T

Design compressive strength for the age index specified in IDX1.

FCD1

Uniform strength for uncracked regions corresponding to the age index specified in IDX1.

FCD2

Uniform strength for cracked regions corresponding to the age index specified in IDX1.

K

Strength ratio (ratio between the mean tensile strength and the mean compressive strength).

ECI

Tangent modulus of elasticity for the age index specified in IDX1.

EC

Reduced modulus of elasticity for the age index specified in IDX1.

EC1

Secant modulus of elasticity for the age index specified in IDX1.

EPSC1

Strain for the maximum compressive stress of concrete.

EPSC_LIM

Maximum compressive strain of concrete for the age index specified in IDX1.

EPSCUB

Maximum bending strain for the parabolic-rectangular diagram.

EPSCUC

Maximum compressive strain for the parabolic-rectangular diagram.

EPSCUU

Maximum strain for uniform stress diagram.

TSASSD

Type of stress-strain diagram for structural analysis:

0- User defined, 1- Elastic-linear, 2- Instantaneous loads.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis.

SAEPS

Strain value of the point of the stress-strain diagram of structural analysis specified in IDX1 for the age index specified in IDX2.

SASGM

Stress value of the point of the stress-strain diagram of structural analysis specified in IDX1 for the age index specified in IDX2.

TSDSSD

Type of stress-strain diagram for sections analysis:

 0- User defined, 1- Parabolic-rectangular, 2- Uniform stress.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of the stress-strain diagram specified in IDX1 for the age index specified in IDX2.

SDSGM

Stress value of the point of the stress-strain diagram specified in IDX1 for the age index specified in IDX2.

 

Lab1= CEB_S

~CFGET, Par, MATERIAL, ENTNUM, CEB_S, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of model code CEB-FIP referred to the reinforcement steel. Valid labels are:

Lab2

Description

GAMS

Steel’s safety factor.

FYK

Characteristic yield stress.

FYD

Design yield stress.

FTK

Characteristic tensile strength.

EPSUK

Characteristic elongation at maximum load.

DUCT

Steel’s ductility (characters parameter):

Duct

S

Duct

A

Duct

B

Duct

NONE

TSASSD

Type of stress-strain diagram for structural analysis: 0- User defined, 1- Elastic-linear, 2- Bi-linear.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis.

SAEPS

Strain value of the point of the structural analysis diagram specified in IDX1 (IDX1 = 1, 2,..., NPSASSD).

SASGM

Stress value of the point of the strain-stress diagram of structural analysis specified in IDX1.

TSDSSD

Type of strain-stress diagram for analysis of sections: 0- User defined, 1- Bi-linear.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point of the analysis stress-strain diagram specified in IDX1.

 

Lab1= EHE_C

~CFGET, Par, MATERIAL, ENTNUM, EHE_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Spanish code EHE referred to concrete material. Valid labels are:

Lab2

Description

CETP

Type of cement (characters parameter)

N

Normal hardening concrete.

R

Rapid hardening concrete.

S

Slow hardening concrete.

GAMC

Concrete’s partial safety factor

FCK

Characteristic compressive strength.

FCM

Mean compressive strength.

FCD

Design compressive strength.

FCTM

Mean tensile strength.

FCTK_005

Lower characteristic tensile strength.

FCTK_095

Upper characteristic tensile strength.

EPSC1

Strain of the maximum compressive stress.

EPSCLIM

Maximum compressive strain.

ECI

Tangent modulus elasticity of concrete modulus.

K

Coefficient depending on the type of cement.

BETC

Coefficient depending on concrete’s age for the age index indicated in IDX1.

FCK_J

Characteristic compressive strength of concrete for the age index indicated in IDX1.

FCM_J

Mean compressive strength of concrete for the age ratio indicated in IDX1.

FCD_J

Design compressive strength of concrete for the age ratio indicated in IDX1.

BETT

Coefficient which depends on concrete age for the age index indicated in IDX1.

FCTM_J

Mean concrete tensile strength for the age index indicated in IDX1.

E0J

Initial tangent modulus of elasticity for the age index indicated in IDX1.

EJ

Instantaneous secant modulus of elasticity for the age index indicated in IDX1.

TSASSD

Type of stress-strain diagram for structural analysis:

 0- User defined, 1- Elastic-linear, 2- Instantaneous loads.

NPSASSD

Number of points of the stress-strain diagram of structural analysis.

SAEPS

Strain value of the point of the structural analysis diagram specified in IDX1 (IDX1 = 1, 2,..., NPSASSD).

SASGM

Stress value of the point of the strain-stress diagram of structural analysis specified in IDX1.

TSDSSD

Type of stress-strain diagram for analysis of sections:

0- User defined, 1- Parabolic-rectangular, 2- Bi-linear, 3- Rectangular.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of analysis stress-strain diagram specified in IDX1 for the age index specified in IDX2.

SDSGM

Stress value of the point of the analysis stress-strain diagram specified in IDX1 for the age index specified in IDX2.

 

Lab1= EHE_S

~CFGET, Par, MATERIAL, ENTNUM, EHE_S, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Spanish code EHE referred to reinforcement steel material. Valid labels are:

Lab2

Description

GAMS

Steel partial safety factor.

FYK

Steel characteristic yield stress.

FYD

Design tensile strength.

FYCD

Design compressive strength.

FMAX

Characteristic tensile strength.

EPSMAX

Characteristic elongation at maximum load.

TSASSD

Type of stress-strain diagram for structural analysis: 0- User defined, 1- Elastic-linear, 2- Bi-linear.

NPSASSD

Number of points of the stress-strain diagram of structural analysis

SAEPS

Strain value of the point in the stress-strain diagram of structural analysis specified in IDX1.

SASGM

Stress value of the point in the stress-strain diagram of structural analysis specified in IDX1.

TSDSSD

Type of the stress-strain diagram of structural analysis: 0- User defined, 1- Bi-linear with horizontal top branch, 2- Bi-linear with inclined top branch.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point in the analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point in the analysis stress-strain diagram specified in IDX1.

 

Lab1= EHE_PRES

~CFGET, Par, MATERIAL, ENTNUM, EHE_PRES, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Spanish code EHE referred to prestressed steel material. Valid labels are:

Lab2

Description

GAMS

Prestressed steel partial safety factor.

FMAX

Maximum tensile strength

FPK

Characteristic elastic limit

FPD

Calculus elastic limit

AGER1

Relaxation time 1 (horas).

AGER2

Relaxation time 2 (horas).

R01-60

AGER1 relaxation and 60% of the fmax

R01-70

AGER1 relaxation and 70% of the fmax

R01-80

AGER1 relaxation and 80% of the fmax

R02-60

AGER2 relaxation and 60% of the fmax

R02-70

AGER2 relaxation and 70% of the fmax

R02-80

AGER2 relaxation and 80% of the fmax

TSASSD

Type of stress-strain diagram for structural analysis: 0- User defined, 1- Elastic-linear, 2- Bi-linear, 3- Characteristic diagram.

NPSASSD

Number of points of the stress-strain diagram of structural analysis

SAEPS

Strain value of the point in the stress-strain diagram of structural analysis specified in IDX1.

SASGM

Stress value of the point in the stress-strain diagram of structural analysis specified in IDX1.

TSDSSD

Type of the stress-strain diagram of structural analysis: 0- User defined, 1- Bi-linear with horizontal top branch, 2- Bi-linear with inclined top branch.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point in the analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point in the analysis stress-strain diagram specified in IDX1.

 

Lab1= BS8110_C

~CFGET, Par, MATERIAL, ENTNUM, BS8110_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of British Standard code referred to concrete material. Valid labels are:

Lab2

Description

CETP

Type of cement (characters parameter)

SL

Slowly hardening cements

N

Normal hardening concrete.

R

Rapid hardening concrete.

RS

Rapid hardening high strength cements.

GAMCN

Safety factor for concrete in flexure or axial load

GAMCS

Safety factor for shear strength without shear reinforcement.

FCU

Characteristic 28 day compressive strength.

EPSC1

Strain in concrete at maximum stress.

EPSCU

Ultimate strain in compression.

S

Coefficient which depends on type of cement.

BETCC

Coefficient depending on concrete’s age for the age index indicated in IDX1.

FCU_T

Characteristic compressive strength for the age index indicated in IDX1.

KO

Constant related to the modulus of elasticity of the aggregate.

EC28

Modulus of elasticity at 28 days.

EC_T

Tangent modulus of elasticity for the age index indicated in IDX1.

TSASSD

Type of stress-strain diagram for structural analysis:

0- User defined, 1- Elastic-linear, 2- Structural analysis.

NPSASSD

Number of points of the stress-strain diagram of structural analysis.

SAEPS

Strain value of the point of the structural analysis diagram specified in IDX1 (IDX1 = 1, 2,..., NPSASSD).

SASGM

Stress value of the point of the strain-stress diagram of structural analysis specified in IDX1.

TSDSSD

Type of stress-strain diagram for analysis of sections:

0- User defined, 1- Parabolic-rectangular, 2- Rectangular.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of analysis stress-strain diagram specified in IDX1 for the age index specified in IDX2.

SDSGM

Stress value of the point of the analysis stress-strain diagram specified in IDX1 for the age index specified in IDX2.

 

Lab1= BS8110_S

~CFGET, Par, MATERIAL, ENTNUM, BS8110_S, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of British Standard code referred to reinforcement steel material. Valid labels are:

Lab2

Description

GAMS

Steel partial safety factor.

FY

Steel characteristic yield stress.

RM

Characteristic tensile strength.

A5

Elongation at fracture.

TSASSD

Type of stress-strain diagram for structural analysis: 0- User defined, 1- Elastic-linear, 2- Bi-linear.

NPSASSD

Number of points of the stress-strain diagram of structural analysis

SAEPS

Strain value of the point in the stress-strain diagram of structural analysis specified in IDX1.

SASGM

Stress value of the point in the stress-strain diagram of structural analysis specified in IDX1.

TSDSSD

Type of the stress-strain diagram of structural analysis: 0- User defined, 1- Bi-linear.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point in the analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point in the analysis stress-strain diagram specified in IDX1.

 

Lab1= GBMAT_C

~CFGET, Par, MATERIAL, ENTNUM, GBMAT_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Chinese code GB50010 referred to concrete material. Valid labels are:

Lab2

Description

CETP

Type of cement:

SL

Slow hardening cements.

N

Normal hardening cements. By default.

R

Rapid hardening cements.

RS

Rapid hardening high strength cements.

GAMC

Partial safety factor for concrete.

FCUK

Standard 28-day compressive strength (cube strength).

ALPC1

Prism strength and cube strength ratio.

ALPC2

Brittle reduction coefficient.

DELTA

Coefficient:

FCK

Standard axial compressive strength.

FC

Design value for axial compressive strength:

FC

≥ 0

FCD

FCK / GAMc

FTK

Standard tensile strength.

FT

Design value for tensile strength.

S

Coefficient which depends on type of cement:

BETCC

Coefficient that depends on concrete age. The age index must be specified in IDX1.

Fck_t

Standard t day compressive strength. The age index must be specified in IDX1.

Fc_t

Design t day compressive strength. The age index must be specified in IDX1.

Ec_t

Modulus of elasticity. The age index must be specified in IDX1.

N

Exponent of the stress strain diagram.

EPS0

Compressive strain at fc.

EPSCU

Limit compressive strain in concrete.

TSASSD

Type of stress-strain diagram for structural analysis: 0- User defined, 1- Elastic-linear, 2- Structural analysis.

SAEPS

Strain value of the point of the structural analysis diagram specified in IDX1 (IDX1 = 1, 2,..., NPSASSD).

SASGM

Stress value of the point of the strain-stress diagram of structural analysis specified in IDX1.

TSDSSD

Type of stress-strain diagram for analysis of sections:

0- User defined, 1- Parabolic-rectangular.

 

Lab1= GBMAT_S

~CFGET, Par, MATERIAL, ENTNUM, GBMAT_S, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of Chinese code GB50010 referred to reinforcement steel material. Valid labels are:

Lab2

Description

GAMS

Safety factor for steel

FYK

Characteristic yield stress

FY

Design tensile strength

TSASSD

Type of stress-strain diagram for structural analysis: 0- User defined, 1- Elastic-linear, 2- Bi-linear

SAEPS

Strain value of the point in the stress-strain diagram of structural analysis specified in IDX1.

SASGM

Stress value of the point in the stress-strain diagram of structural analysis specified in IDX1.

TSDSSD

Type of stress-strain diagram for section’s analysis: 0- User defined, 1- Bi-linear.

SDEPS

Strain value of the point in the analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point in the analysis stress-strain diagram specified in IDX1.

 

Lab1= NBR_C

~CFGET, Par, MATERIAL, ENTNUM, NBR_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data referred to NBR6118 concrete material. Valid labels are:

Lab2

Description

CETP

Type of cement.

S

Slow hardening cements

N

Normal hardening cements

R

Rapid hardening cements

RS

Rapid hardening-high strength cements

GAMC

Partial safety factor for concrete.

FCK

Characteristic 28-day compressive strength.

FCM

Mean 28-day compressive strength.

FCD

Design 28-day compressive strength.

FCTM

Mean tensile strength.

FCTK_INF

Lower characteristic tensile strength.

FCTK_SUP

Upper characteristic tensile strength.

SD

Standard deviation.

S

Coefficient which depends on the type of cement.

BET1

Coefficient which depends on concrete age for the age index specified in IDX1.

FCM_J

Mean j day compressive strength corresponding to the age index indicated in IDX1.

FCK_J

Characteristic compressive strength corresponding to the age ratio indicated in IDX1.

FCD_J

Design compressive strength corresponding to the age ratio indicated in IDX1.

ECS

Secant modulus of elasticity corresponding to the age ratio indicated in IDX1.

ECI

Initial modulus of elasticity corresponding to the age ratio indicated in IDX1.

TSASSD

Type of stress-strain diagram for structural analysis:

 0- User Defined, 1- Elastic-linear.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the age index indicated in IDX2.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the age index indicated in IDX2

TSDSSD

Type of the stress-strain diagram for analysis of sections: 0- User defined, 1-Parabolic-rectangular.

NPSDSSD

Number of points of the stress-strain diagram of the analysis of sections.

SDEPS

Strain value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the age index indicated in IDX2.

SDSGM

Stress value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the age index indicated in IDX2.

 

Lab1= NBR_S

~CFGET, Par, MATERIAL, ENTNUM, NBR_S, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of NBR6118 referred to reinforcement steel material. Valid labels are:

Lab2

Description

GAMS

Steel’s safety factor.

FYK

Characteristic yield stress.

FYD

Design yield stress.

FSTK

Characteristic tensile strength.

EPSUK

Characteristic elongation at maximum load.

TSASSD

Type of stress-strain diagram of structural analysis:

0- User defined, 1- Elastic-linear, 2- Characteristic Diagram.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis.

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

TSDSSD

Type of strain-stress diagram for analysis of sections: 0- User defined, 1- Design diagram.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point of the analysis stress-strain diagram specified in IDX1.

 

Lab1= IS_C

~CFGET, Par, MATERIAL, ENTNUM, IS_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data referred to IS456 concrete material. Valid labels are:

Lab2

Description

CETP

Type of cement.

SL

Slow hardening cements.

N

Normal hardening cements. Default value

R

Rapid hardening cements

RS

Rapid hardening high strength cements

GAMC

Partial safety factor for concrete.

FCK

Characteristic 28-day compressive strength.

FCD

Design 28-day compressive strength.

FCT

Characteristic tensile strength.

S

Coefficient which depends on the type of cement.

BETCC

Coefficient which depends on concrete age for the age index specified in IDX1.

FCK_T

Characteristic t day compressive strength.

FCD_T

Design t day compressive strength.

EC

Modulus of elasticity at 28 days.

EC_T

Modulus of elasticity.

TSASSD

Type of stress-strain diagram for structural analysis:

 0- User Defined, 1- Elastic-linear.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the age index indicated in IDX2.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the age index indicated in IDX2

TSDSSD

Type of the stress-strain diagram for analysis of sections: 0- User defined, 1-Parabolic-rectangular.

NPSDSSD

Number of points of the stress-strain diagram of the analysis of sections.

SDEPS

Strain value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the age index indicated in IDX2.

SDSGM

Stress value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the age index indicated in IDX2.

 

Lab1= IS_S

~CFGET, Par, MATERIAL, ENTNUM, IS_S, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of IS456 referred to reinforcement steel material. Valid labels are:

Lab2

Description

GAMS

Steel’s safety factor.

FY

Characteristic yield stress.

FYD

Design yield stress.

FT

Characteristic tensile strength.

EPSUK

Characteristic elongation at maximum load.

TSASSD

Type of stress-strain diagram of structural analysis:

0- User defined, 1- Elastic-linear, 2- Bi-linear.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis.

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

TSDSSD

Type of strain-stress diagram for analysis of sections: 0- User defined, 1- Bi-linear.

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point of the analysis stress-strain diagram specified in IDX1.

 

Lab1= SP_C

~CFGET, Par, MATERIAL, ENTNUM, SP_C, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data referred to SP52101 or SP63.13330 concrete material. Valid labels are:

Lab2

Description

CETP

Type of cement.

SL

Slow hardening cements.

N

Normal hardening cements. Default value

R

Rapid hardening cements

RS

Rapid hardening high strength cements

GAMB

Partial safety factor for concrete (compression)

GAMBT

Partial safety factor for concrete (tension)

RBN

Characteristic 28-day compressive strength.

RB

Design 28-day compressive strength.

RBTN

Characteristic 28 day tensile strength.

RBN_T

Characteristic t day compressive strength.

RB_T

Design t day compressive strength.

EB

Initial modulus of elasticity

EPSB1

Strain at the end of the first segment of the strain-stress curve.

EPSB0

Strain at the end of the second segment of the strain-stress curve.

EPSB2

Ultimate strain in compression.

EPSB1_RED

Reduced EPSB1 for the bi-linear diagram.

S

Coefficient which depends on the type of cement.

BETCC

Coefficient which depends on concrete age for the age index specified in IDX1.

TSASSD

Type of stress-strain diagram for structural analysis:

 0- User Defined, 1- Elastic-linear, 2- Bi-linear, 3- Tri-linear.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the age index indicated in IDX2.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1 for the age index indicated in IDX2

TSDSSD

Type of the stress-strain diagram for analysis of sections: 0- User defined, 1- Bi-linear, 2- Tri-linear.

NPSDSSD

Number of points of the stress-strain diagram of the analysis of sections.

SDEPS

Strain value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the age index indicated in IDX2.

SDSGM

Stress value of a point of the stress-strain diagram corresponding to the section’s analysis specified in IDX1 for the age index indicated in IDX2.

 

Lab1= SP_S

~CFGET, Par, MATERIAL, ENTNUM, SP_S, Lab2, , IDX1, IDX2, IDX3

Retrieves specific data of SP52101 or SP 63.13330 referred to reinforcement steel material. Valid labels are:

Lab2

Description

GAMS

Steel’s safety factor.

RSN

Characteristic yield stress.

RS

Design tensile strength.

RSW

Design yield stress of stirrups.

EPSS2

Characteristic elongation at maximum load.

TSASSD

Type of stress-strain diagram of structural analysis:

0- User defined, 1- Elastic-linear, 2- Bi-linear, 3- Tri-linear.

NPSASSD

Number of points of the stress-strain diagram of the structural analysis.

SAEPS

Strain value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

SASGM

Stress value of a point of the stress-strain diagram corresponding to the structural analysis specified in IDX1.

TSDSSD

Type of strain-stress diagram for analysis of sections: 0- User defined, 1- Bi-linear, 2- Tri-linear .

NPSDSSD

Number of points of the analysis stress-strain diagram.

SDEPS

Strain value of the point of analysis stress-strain diagram specified in IDX1.

SDSGM

Stress value of the point of the analysis stress-strain diagram specified in IDX1.

 

Lab1= FLZONE

~CFGET, Par, MATERIAL, ENTNUM, FLZONE, Lab2, Lab3, IDX1, IDX2, IDX3

Retrieves FLAC material properties for soil and rock elements. Valid labels are:

Lab2

Lab3

Description

CMOD

 

Type of constitutive model

1

Null model

2

Elastic isotropic (default)

3

Elastic orthotropic

4

Elastic transversely isotropic

5

Drucker-Prager

6

Mohr-Coulomb

7

Ubiquitous-joint

8

Strain-hardening/softening

9

Bilinear strain-hard/soft ubiquitous-joint

10

Double-yield

11

Modified Cam-Clay

ISO

bu

Elastic bulk modulus, K

 

sh

Elastic shear modulus, G

ORT

dd

Dip direction of plane defined by axes 1'-2'

 

dip

Dip angle of plane defined by axes 1'-2'

 

e1

Young's modulus in direction 1'

 

e2

Young's modulus in direction 2'

 

e3

Young's modulus in direction 3'

 

g12

Shear modulus in planes parallel to axes 1'-2'

 

g13

Shear modulus in planes parallel to axes 1'-3'

 

g23

Shear modulus in planes parallel to axes 2'-3'

 

nu12

Poisson´s ratio characterizing lateral contraction in direction 1' when tension is applied in direction 2'

 

nu13

Poisson´s ratio characterizing lateral contraction in direction 1' when tension is applied in direction 3'

 

nu23

Poisson´s ratio characterizing lateral contraction in direction 2' when tension is applied in direction 3'

 

nx

x-component of unit normal to plane defined by axes 1'-2'

 

ny

y-component of unit normal to plane defined by axes 1'-2'

 

nz

z-component of unit normal to plane defined by axes 1'-2'

 

rot

Rotation angle between the 1' axis and the dip-direction vector, defined positive clockwise from the dip-direction vector

TRA

dd

Dip direction of plane of isotropy

 

Dip

Dip angle of plane of isotropy

 

E1

Young's modulus in the plane of isotropy

 

E3

Young's modulus normal to the plane of isotropy

 

G13

Shear modulus for any plane normal to the plane of isotropy

 

Nu12

Poisson´s ratio characterizing lateral contraction in the plane of isotropy when tension is applied in the plane

 

Nu13

Poisson´s ratio characterizing lateral contraction in the plane of isotropy when tension is applied normal to the plane

DP

Bu

Elastic bulk modulus, K

 

Ks

Material parameter, phi

 

Qd

Material parameter,qpsi

 

Qv

Material parameter, phi

 

Sh

Elastic shear modulus, G

 

ten

Tension limit, SIGt

MC

bu

Elastic bulk modulus, K

 

C

Cohesion, c

 

Di

Dilation angle, psi

 

Fric

Internal angle of friction, phi

 

Sh

Elastic shear modulus, G

 

ten

Tension limit, SIGt

UJ

bu

Elastic bulk modulus, K

 

C

Cohesion of matrix, c

 

Di

Dilation angle of matrix, psi

 

Fric

Internal angle of friction, phi

 

Jc

Joint cohesion, cj

 

Jdd

Dip direction of weakness plane

 

Jdil

Joint dilation angle, psij

 

Jdip

Dip angle of weakness plane

 

Jf

Joint friction angle, phij

 

Jnx

x-component of unit normal to weakness plane

 

Jny

y-component of unit normal to weakness plane

 

Jnz

z-component of unit normal to weakness plane

 

Jt

Joint tension limit, SIGtj

 

Sh

Elastic shear modulus, G

 

ten

Tension limit of matrix, SIGt

HS

bu

Elastic bulk modulus, K

 

C

Cohesion, c

 

Ct

Number of table relating cohesion to plastic shear strain

 

Di

Dilation angle, psi

 

Dt

Number of table relating dilation angle to plastic shear strain

 

Fric

Angle of internal friction, phi

 

Ft

Number of table relating friction angle to plastic shear strain

 

Sh

Elastic shear modulus, G

 

Ten

Tension limit, SIGt

 

tt

Number of table relating tension limit to plastic tensil strain

BHS

Bij

=0 for joint linear model

=1 for joint bilinear model

 

Bim

=0 for matrix linear model

=1 for matrix bilinear model

 

bu

Elastic bulk modulus, K

 

C2

Number of table relating matrix cohesion c2 to matrix plastic shear strain

 

Cj

Number of table relating joint cohesion cj1 to joint plastic shear strain

 

Cj2

Number of table relating joint cohesion cj2 to joint plastic shear strain

 

C

Matrix cohesion, c1

 

Co2

Matrix cohesion, c2

 

Ct

Number of table relating matrix cohesion c1 to matrix plastic shear strain

 

D2

Number of table relating matrix dilation psi2 to matrix plastic shear strain

 

Di2

Matrix dilation angle, psi2

 

Di

Matrix dilation angle, psi1

 

Dj

Number of table relating joint dilation psij1 to joint plastic shear strain

 

Dj2

Number of table relating joint dilation psij2 to joint plastic shear strain

 

Dt

Number of table relating matrix dilation angle psi1 to matrix plastic shear strain

 

F2

Number of table relating matrix friction angle phi2 to matrix plastic shear strain

 

Fj

Number of table relating joint friction angle phij1 to joint plastic shear strain

 

Fj2

Number of table relating joint friction angle phij2 to joint plastic shear strain

 

Fr2

Matrix friction angle, phi2

 

Fric

Matrix friction angle, phi1

 

Ft

Number of table relating matrix friction phi1 to matrix plastic shear strain

 

Jc2

Joint cohesion,cj2

 

Jc

Joint cohesion,cj1

 

Jdd

Dip direction of weakness plane

 

Jdil

Joint dilation angle, psij1

 

Jdip

Dip angle of weakness plane

 

Jd2

Joint dilation angle, psij2

 

Jf

Joint friction angle, phij1

 

Jf2

Joint friction angle, phij2

 

Jnx

x-component of unit normal to weakness plane

 

Jny

y-component of unit normal to weakness plane

 

Jnz

z-component of unit normal to weakness plane

 

Jt

Joint tension limit, SIGtj

 

Sh

Elastic shear modulus, G

 

Ten

Matrix tension limit,SIGt

 

Tj

Number of table relating joint tension limit SIGtj to joint plastic tensile strain

 

Tt

Number of table relating matrix tension limit SIGtj to joint plastic tensile strain

DY

Bu

Elastic bulk modulus, K

 

Cap_p

Current intersection of volumetric yield surface (cap) with pressure (mean stress) axis, pc

 

C

Cohesion, c

 

Cp

Number of table relating cap pressure to plastic volume strain

 

Ct

Number of table relating cohesion to plastic shear strain

 

Di

Dilation angle, psi

 

Dt

Number of table relating dilation angle to plastic shear strain

 

Ev

Accumulated plastic volumetric strain

 

F

Angle of internal friction, phi

 

Ft

Number of table relating friction angle to plastic shear strain

 

Mu

Multiplier on current plastic cap modulus to give elastic bulk and shear module, R

 

S

Maximum elastic shear modulus, G

 

T

Tension limit, SIGt

 

tt

Number of table relating tensile limit to plastic tensile strain

CC

Bulk_b

Maximum elastic bulk modulus, kmax

 

Cv

Initial specific volume, v0

 

Ka

Slope of elastic swelling line, kappa

 

L

Slope of normal consolidation line, lambda

 

Mm

Frictional constant, M

 

Mpc

Preconsolidation pressure, pc0

 

Mp1

Reference pressure, p1

 

Mv_l

Specific volume at reference pressure, p1, on normal consolidation line, vlambda

 

P

Poisson's ratio, nu

 

sh

Elastic shear modulus, G

 

Lab1= FLSEL

~CFGET, Par, MATERIAL, ENTNUM, FLSEL, Lab2, Lab3, IDX1, IDX2, IDX3

Retrieves FLAC material properties for structural elements. Valid labels are:

Lab2

Lab3

Description

TSEL

 

Type of structural element

1

BeamSEL (default option)

2

CableSEL

3

PileSEL

4

ShellSEL

5

GeogridSEL

6

LinerSEL

BEAM

density

Mass density, ro

 

emod

Young's modulus, E

 

Nu

Poisson's ratio, nu

 

pmoment

Plastic moment capacity, Mp

 

thexp

Thermal expansion coefficient, alphat

CABLE

density

Mass density, ro

 

Emod

Young's modulus, E

 

Gr_coh

Grout cohesive strength (force) per unit of length, cg

 

Gr_fric

Grout friction angle, phig (º)

 

Gr_k

Grout stiffness per unit length, kg

 

Gr_per

Grout exposed perimeter, pg

 

Slide

Large-strain sliding flag (default: OFF)

 

Slide_to

Large-strain sliding tolerance

 

Thexp

Thermal expansion coefficient, alphat

 

Ycomp

Compressive yield stength (force), Fc

 

ytens

Tensile yield strength (force), Ft

PILE

Density

Mass density, ro

 

Emod

Young's modulus, E

 

Nu

Poisson's ratio, nu

 

Pmoment

Plastic moment capacity, Mp

 

Thexp

Thermal expansion coefficient, alphat

 

Cs_scoh

Shear coupling spring cohesion per unit length, cs

 

Cs_sfric

Shear coupling spring friction angle, Phis (º)

 

Cs_sk

Shear coupling spring stiffness per unit length, ks

 

Cs_ncoh

Normal coupling spring cohesion per unit length, cn

 

Cs_nfric

Normal coupling spring friction angle, phin (º)

 

Cs_ngap

Normal coupling spring gap-use flag, g (default: OFF)

 

Cs_nk

Normal coupling stiffness per unit length, kn

 

Slide

Large-strain sliding flag

 

Slide_to

Large-strain sliding tolerance

SHELL

Tbeh

Type of constitutive behavior

1

Isotropic (default option)

2

Orthotropic

 

Ele

Finite element type

1

CST

2

CSTH

3

DKT

4

DKT_CST

5

DKT_CSTH

 

Density

Mass density, ro

 

Emod

Young's modulus, E (Isotropic)

 

Nu

Poisson's ratio, nu (Isotropic)

 

E11

Orthotropic material property, e11

 

E12

Orthotropic material property, e12

 

E22

Orthotropic material property, e22

 

E33

Orthotropic material property, e33

 

Thexp

Thermal expansion coefficient, alphat

GEOG

Tbeh

Type of constitutive behavior

1

Isotropic (default option)

2

Orthotropic

 

Ele

Finite element type

1

CST

2

CSTH

3

DKT

4

DKT_CST

5

DKT_CSTH

 

Density

Mass density, ro

 

Emod

Young's modulus, E (Isotropic)

 

Nu

Poisson's ratio, nu (Isotropic)

 

E11

Orthotropic material property e11

 

E12

Orthotropic material property e12

 

E22

Orthotropic material property e22

 

E33

Orthotropic material property e33

 

Thexp

Thermal expansion coefficient, alphat

 

Cs_scoh

Coupling spring cohesion (stress units), c

 

Cs_sfric

Coupling spring friction angle, phi (º)

 

Cs_sk

Coupling spring stiffness per unit area, k

 

Slide

Large-strain sliding flag (default: OFF)

 

Slide_to

Large-strain sliding tolerance

LINER

Tbeh

Type of constitutive behavior

1

Isotropic (default option)

2

Orthotropic

 

Ele

Finite element type

1

CST

2

CSTH

3

DKT

4

DKT_CST

5

DKT_CSTH

 

Density

Mass density, ro

 

Emod

Young's modulus, E (Isotropic)

 

Nu

Poisson's ratio, nu (Isotropic)

 

E11

Orthotropic material property e11

 

E12

Orthotropic material property e12

 

E22

Orthotropic material property e22

 

E33

Orthotropic material property e33

 

Thexp

Thermal expansion coefficient, alphat

 

Cs_ncut

Normal coupling spring tensile strength (stress units), ft

 

Cs_nk

Normal coupling spring stiffness per unit area, kn

 

Cs_scoh

Shear coupling spring cohesion (stress units), c

 

Cs_scohr

Shear coupling spring residual cohesion (stress units), cr

 

Cs_sfric

Shear coupling spring friction angle, phi (º)

 

Cs_sk

Shear coupling spring stiffness per unit area, ks

 

Slide

Large-strain sliding flag (default: OFF)

 

Slide_to

Large-strain sliding tolerance

 

Lab1= SOIL

~CFGET, Par, MATERIAL, ENTNUM, SOIL, Lab2, , IDX1, IDX2, IDX3

Retrieves soil material properties. Valid labels are:

Lab2

Description

TpEx

Type of Ex used in structural analysis:

1

Static elasticity modulus (default option).

2

Dynamic modulus.

TpNUxy

Type of Poisson coefficient used in structural analysis:

1

Static Poison’s ratio.

2

Dynamic Poison’s ratio.

TpRHO

Type of Density used in structural analysis:

1

Bulk density (default option).

2

Submerged density.

KPLA

Type of behavior:

0

Elastic

1

Drucker-Prager

2

Mohr-Coulomb

3

Cam-Clay

ExSt

Static elasticity modulus

NUxySt

Static Poisson modulus

Vp

P waves velocity

Vs

S waves velocity

Exd

Dynamic elasticity modulus

Nuxyd

Dynamic Poisson modulus

GAMd

Dry specific weight

GAMw

Water specific weight

RHOrel

Relative density

n

Porosity

W

Moisture content.

D10

Diameter that allows more than 10% of material to pass (in millimeters).

D30

Diameter that allows more than 30% of material to pass (in millimeters).

D60

Diameter that allows more than 60% of material to pass (in millimeters).

SPT

Standard penetration test.

CPT

Cone penetration test.

Qu

Resistance to simple compression.

Em

Edometric modulus.

Qa

Maximum admissible load.

Wl

Liquid limit percentage

wp

Plastic limit percentage

PHIMCeff

Angle of effective internal resistance for Mohr-Coulomb (in degrees).

cMCeff

Effective cohesion for Mohr-Coulomb

PHIDPeff

Angle of effective internal resistance for Drucker-Prager

cDPeff

Effective cohesion for Drucker-Prager.

DELeff

Dilation.

K0

Pressure coefficient at rest.

Ka

Active pressure coefficient.

Kp

Passive pressure coefficient.

Kac

Cohesion complementary component of active pressure.

Kpc

Cohesion complementary component of passive pressure.

RuSI

Susceptibility to pore pressure:

0

Not susceptible

1

Susceptible

Ru

Coefficient for pore pressure after consolidation.

Kx

Permeability X.

ky

Permeability Y.

kz

Permeability Z.

cv

Consolidation coefficient.

A

Skempton law’s coefficient.

B

Skempton law’s coefficient.

BET

Skempton law’s coefficient.

KMCSP

Way of specifying the shape parameters HYP and ECC for Mohr-Coulomb yield surface:

0

Auto calculated (default)

1

User values

IFLOW

Type of flow rule in Mohr-Coulomb plasticity model:

0

Associated flow

1

Non associated flow

HYP

Hyperbolicity parameter in Mohr-Coulomb yield surface.

ECC

Eccentricity parameter in Mohr-Coulomb yield surface

(0.55 ≤ ECC ≤ 1).

KP0

Way of specifying the preconsolidation:

0

Through the overconsolidation ratio OCR.

1

Through the initial preconsolidation pressure P0.

M

Slope of the critical state line in the q-p plane.

LAM

Slope of the isotropic compression line in v-ln(p) plane.

KAP

Slope of the unloading-reloading line in v-ln(p) plane.

VICL

Specific volume at unit pressure in isotropic compression.

P0

Initial preconsolidation pressure.

 

Lab1= ROCK

~CFGET, Par, MATERIAL, ENTNUM, ROCK, Lab2, , IDX1, IDX2, IDX3

Retrieves rock material properties. Valid labels are:

Lab2

Description

TpEx

Type of elasticity module used in structural analysis:

1

Static modulus of elasticity (by default).

2

Dynamic modulus of elasticity.

TpNUxy

Type of Poison’s ratio coefficient used in structural analysis:

1

Static Poison’s ratio.

2

Dynamic Poison’s ratio.

TpRHO

Type of Density used in structural analysis:

1

Bulk density (default option).

2

Submerged density.

KPLA

Type of behavior:

0

Elastic

1

Drucker-Prager

2

Mohr-Coulomb

ExSt

Static elasticity modulus

NUxySt

Static Poisson modulus

Vp

P waves velocity

Vs

S waves velocity

Exd

Dynamic elasticity modulus

NUxyd

Dynamic Poisson modulus

qu

Resistance to simple compression.

GAMd

Dry specific weight

GAMw

Water specific weight

RHOrel

Relative density (by default 0.5)

n

Porosity

W

Moisture content.

PHIeff

Angle of internal effective resistance (degrees).

ceff

Effective cohesion.

PHIDPeff

Angle of internal effective resistance for Drucker-Prager (degrees)

cDPeff

Effective cohesion for Drucker-Prager.

DELeff

Dilation (degrees).

K0

Pressure coefficient at rest.

Ka

Active pressure coefficient.

Kp

Passive pressure coefficient.

Kac

Cohesion complementary component of active pressure.

Kpc

Cohesion complementary component of passive pressure.

RuSI

Susceptibility to pore pressure:

0

Not susceptible.

1

Susceptible.

Ru

Coefficient for pore pressure after consolidation.

kx

Permeability X.

ky

Permeability Y.

kz

Permeability Z.

GSI

Geological strength index.

HB_m

Hoek & Brown coefficient m

HB_s

Hoek & Brown coefficient s

HB_mr

Hoek & Brown residual coefficient m

HB_sr

Hoek & Brown residual coefficient s

HB_n

Hoek & Brown coefficient n.

HB_m0

Hoek & Brown coefficient m for unfractured rock.

HB_s0

Hoek & Brown coefficient s for unfractured rock.

HB_ALF

Fragility / ductility limit coefficient.

HB_md

Factor for dilatancy calculation.

HB_bd

Factor for dilatancy calculation.

KMCSP

Way of specifying the shape parameters HYP and ECC for Mohr-Coulomb yield surface:

0

Auto calculated (default)

1

User values

IFLOW

Type of flow rule in Mohr-Coulomb plasticity model:

0

Associated flow

1

Non associated flow

HYP

Hyperbolicity parameter in Mohr-Coulomb yield surface.

ECC

Eccentricity parameter in Mohr-Coulomb yield surface

(0.55 ≤ ECC ≤ 1)

 

·         ~CFGET – SECTION (ENTNUM = Number of cross section)

 

~CFGET, Par, SECTION, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= PROPGEN

~CFGET, Par, SECTION, ENTNUM, PROPGEN, Lab2, , IDX1, IDX2, IDX3

Retrieves common general properties to all cross sections. Valid labels are:

 

Lab2

Description

RF16

Cross-section reference (parameter of 16 characters). In hot rolled sections is the library reference and in the rest of sections is a STP (section type) label dependent.

NAME

Name assigned to cross-section (32 characters). IDX1 indicates the group of 8 characters to retrieve.

IDX1

Group of characters

1

1 to 8

2

9 to 16

3

17 to 24

4

25 to 32

STP

Type of cross section

0

Generic

1

Structural steel

2

Reinforced concrete

3

Concrete + Steel

SHP

Topology of section

0

Generic

1

Double T

2

Channel

3

Pipe

4

Angle

5

Square / Rectangular

6

Tubular Square / Box

7

Circular

8

Simple T

CSYS

Section coordinate system number.

COOR

 X, Y, Z coordinates of the origin of the coordinates system of the section with respect to the global system. In IDX1 it must be specified which of the 3 components is to be obtained (1:X, 2:Y, 3:Z).

ANGL

THXY, THYZ, THZX rotation angles of the coordinates system of the section with respect to the global system. In IDX1 it must be specified which of the 3 components is to be obtained (1:THXY, 2:THYZ, 3:THZX).

MCOS

Total cost of all section’s materials per unit length.

SCOS

Additional cost per unit surface area.

LCOS

Additional cost per unit length.

PERM

Perimeter of the section subject to SCOS.

TCOS

Total cost per unit length. The stored value is the summation of (MCOS+SCOS*PERM+LCOS).

NPT

Number of points of the section.

NTS

Number of tessella in the section.

NPL

Number of plates of the section.

NFC

Number of faces of the section.

NRB

Number of groups of bending reinforcements defined in the section.

 

Lab1= DIMENS

~CFGET, Par, SECTION, ENTNUM, DIMENS, Lab2, , IDX1, IDX2, IDX3

Retrieves the dimensions of the cross sections. They are only used in sections defined by dimensions or from the library. The meaning of each data depends on each section in particular. Values to retrieve (defined in field IDX1) for hot rolled and welded steel sections are:

IDX1

Description

1

Depth of section (h).

2

Web thickness (Tw).

3

Width of section (b).

4

Flange thickness (Tf).

5

Depth between flanges (hi).

6

Weld throat thickness (for welded sections) / radius of fillet (for hot rolled sections)

7

Toe radius (r2).

8

Depth between fillets (d)

 

Valid values(defined in field IDX1) for circular solid, hot rolled or reinforced sections are:

IDX1

Description

1

Diameter (OD).

 

Valid values (defined in field IDX1) for hollow, hot rolled or reinforced sections are:

IDX1

Description

1

Diameter (OD).

2

Wall thickness (TKWALL).

 

In concrete sections valid values depend on the type of the section. For a box section (BOX) are the following:

IDX1

Description

1

Y width (Tky).

2

Z width (Tkz).

3

Y thickness (Twy).

4

Z thickness (Twz).

 

For a circular concrete section (CIRC) the values are the following:

IDX1

Description

1

Diameter (OD)

2

Number of cells (Ncells) for Beam 188 and Beam 189 elements. Not used for the rest of elements.

 

For a concrete Double T section (I) are the following:

IDX1

Description

1

Total depth (Depth).

2

Web thickness (Tw).

3

Top flange width (BfTop).

4

Top flange thickness (TfTop).

5

Bottom flange width (BfBot).

6

Bottom flange width (TfBot).

 

For a concrete circular annular section (PIPE) are the following:

IDX1

Description

1

Diameter (OD).

2

Wall thickness (TKWALL).

3

Number of cells (Ncells) for Beam 188 and Beam 189 elements. It is ignored for the rest of elements.

 

For a concrete rectangular section (REC) are:

IDX1

Description

1

Y width (Tky).

2

Z width (Tkz).

3

Number of cells (NB) over the width (for Beam 188 and 189 elements).

4

Number of cells (NH) over the depth (for Beam 188 and 189 elements).

 

For a concrete T section (T) are:

IDX1

Description

1

Total depth (Depth).

2

Web thickness (Tw).

3

Flange width (Bf).

4

Top flange thickness (Tf).

 

Lab1= POINTS

~CFGET, Par, SECTION, ENTNUM, POINTS, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the points of cross sections. Valid labels are:

Lab2

Description

Y

Y coordinate of the point specified in IDX1. The inverse function can be found in the ~CSIQR command.

Z

Z coordinate of the point specified in IDX1. The inverse function can be found in the ~CSIQR command.

MAT

Number of the material associated to the specified point in IDX1.

MTP

Type of material associated to the point specified in IDX1.

0

Generic

1

Structural Steel

2

Concrete

3

Reinforcing Steel

NOD

Number of node associated to the point specified in IDX1. It retrieves a 0 in case there is no node associated.

 

Lab1= TESSELLA

~CFGET, Par, SECTION, ENTNUM, TESSELLA, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to tessella of cross sections. Valid labels are:

Lab2

Description

MAT

Number of material associated to the tessellum specified in IDX1.

MTP

Type of the material associated to the tessellum specified in IDX1.

0

Generic

1

Structural Steel

2

Concrete

3

Reinforcing Steel

TYP

Type of tessellum specified in IDX1.

1

Point.

2

Linear of 2 nodes.

3

Linear of 3 nodes.

4

Triangular with 3 nodes.

5

Triangular with 6 nodes.

6

Quadrangular with 4 nodes.

7

Quadrangular with 8 nodes.

TPT

Number of the point of the tessellum specified in IDX1 in IDX2 position.

ELM

Number of element associated to the tessellum specified in IDX1. In case there is no element associated, a 0 is retrieved.

EFN

Number of face or node associated to the tessellum specified in IDX1. If the tessellum is not associated to any face or node, a 0 is retrieved.

RNF

Number of the bending reinforcement group associated to the tessellum specified in IDX1. If the tessellum is not associated to any group, a 0 is retrieved.

PLT

Number of the plate associated to the tessellum specified in IDX1. If the tessellum is not associated to any plate, a 0 is retrieved.

GEO

Additional geometric data of the tessellum specified in IDX1. For punctual tessella:

IDX2 = 1

Tessellum area

IDX2 = 2

0

For linear tessellum:

IDX2 = 1

Tessellum thickness (i end).

IDX2 = 2

Tessellum thickness (j end).

 

Lab1= PLATES

~CFGET, Par, SECTION, ENTNUM, PLATES, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to plates of cross sections. Valid labels are:

Lab2

Description

MAT

Number of material associated to the plate specified in IDX1.

MTP

Type of material associated to the plate specified in IDX1.

0

Generic

1

Structural steel

2

Concrete

3

Reinforcement steel

PTY

Type of plate for My bending of the specified plate in IDX1.

0

Non defined

1

Flange

2

Web

PTZ

Type of plate for Mz bending in IDX1.

0

Non defined

1

Flange

2

Web

CP1

Connection condition in point 1 of the plate specified in IDX1.

0

Free

1

Fixed

CP2

Connection condition in point 2 of the plate specified in IDX1.

0

Free

1

Fixed

ESP

Thickness of the plate specified in IDX1.

YP1

Y coordinate of point 1 of the plate specified in IDX1.

ZP1

Z coordinate of point 1 of the plate specified in IDX1.

YP2

Y coordinate of point 2 of the specified plate in IDX1.

ZP2

Z coordinate of point 2 of the plate specified in IDX1.

 

Lab1= FACES

~CFGET, Par, SECTION, ENTNUM, FACES, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to faces of cross sections. Valid labels are:

Lab2

Description

NPT

Number of points which belong to the face specified in IDX1.

UPT

Number of points which form the face specified in IDX1. In IDX2 the index of the point to be obtained must be specified.

 

Lab1= RNFBEN

~CFGET, Par, SECTION, ENTNUM, RNFBEN, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to groups of bending reinforcements of cross sections. Valid labels are:

Lab2

Description

RKEY

Initial bending reinforcement key.

RMAT

Material number of reinforcement groups defined through initial reinforcement (RKEY>0).

URF

Group number of bending reinforcement specified in IDX1.

MAT

Number of material associated to the reinforcement group specified in IDX1.

CLS

Class of reinforcement group specified in IDX1.

0

If reinforcement is scalable.

1

If reinforcement is fixed.

FI

Diameter of reinforcement bars group specified in IDX1.

UFC

Face number to which is associated the reinforcement group specified in IDX1.

END

Situation of bars in the ends of the face of the reinforcement group specified in IDX1.

0

Bars in both ends of face

1

Bars at end 1 of face

2

Bars at end 2 of face

3

No bars in ends of face.

4

Bars in both ends of face at a distance equal to the mechanical cover (Mc).

MC

Mechanical cover of the reinforcement group specified in IDX1.

GC

Geometric cover of reinforcement group specified in IDX1.

AST

Total area of the reinforcement group specified in IDX1.

ASL

Total area of reinforcement per unit length of the reinforcement group specified in IDX1.

N

Number of bars of the reinforcement group specified in IDX1.

NL

Number of bars per unit length of the reinforcement group specified in IDX1.

S

Distance between bars in the reinforcement group specified in IDX1.

 

Lab1= RNFSHR

~CFGET, Par, SECTION, ENTNUM, RNFSHR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to shear reinforcement of cross sections. Valid labels are:

Lab2

Description

MAT

Material number associated to the shear reinforcement.

ALPY

Angle of the shear Y stirrups with the member’s longitudinal axis.

ALPZ

Angle of the shear Z stirrups with the member’s longitudinal axis.

ASSY

Area of reinforcement per unit length for Y shear.

ASSZ

Area of reinforcement per unit length for Z shear.

ASY

Total area of the stirrup for Y shear.

ASZ

Total area of the stirrup for Z shear.

S

Spacing of stirrups.

FI

Diameter of stirrups bars (in mm).

NY

Number of stirrup legs for Y shear.

NZ

Number of stirrup legs for Z shear.

 

Lab1= RNFTOR

~CFGET, Par, SECTION, ENTNUM, RNFTOR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to torsional reinforcement of cross sections. Valid labels are:

Lab2

Description

MAT

Material number associated to torsional reinforcement.

ASST

Area of transverse reinforcement per unit length.

AST

Area of a stirrup of transverse reinforcement.

S

Longitudinal spacing of stirrups.

FIT

Diameter of bars of transverse reinforcement.

ASL

Total area of transverse reinforcement.

FIL

Diameter of bars of longitudinal reinforcement.

N

Number of bars of longitudinal reinforcement.

 

Lab1= MECHPROP

~CFGET, Par, SECTION, ENTNUM, MECHPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to mechanical properties of cross sections. In IDX1 the set of mechanical properties to be stored between the 8 possible choices must be specified (see CivilFEM Theory Manual for more information). These choices are:

IDX1

Description

1

Gross Generic Section.

2

Steel Gross Section.

3

Steel Net Section.

4

Steel Effective Section.

5

Concrete Gross Section.

6

Concrete Net Section.

7

Concrete Transformed Section.

8

Equivalent Composite Section.

 

In the field corresponding to Lab2 valid labels are:

Lab2

Description

HMAT

Material for which the properties of the sections have been homogenized.

KHOM

Key of homogenization of mechanical properties. Values stored are:

0

Not homogenized.

1

Homogenized with modulus of elasticity.

A

Area of the section.

IXX

Torsional inertia.

IYY

Y axis bending inertia.

IZZ

Z axis bending inertia.

WY

Y elastic resistant modulus.

WZ

Z elastic resistant modulus.

WPY

Y plastic modulus.

WPZ

Z plastic modulus.

IY

Y radius of gyration.

IZ

Z radius of gyration.

YG

Y coordinate of GC.

ZG

Z coordinate of GC.

YMN

Minimum Y coordinate of section boundary.

YMX

Maximum Y coordinate of section boundary.

ZMN

Minimum Z coordinate of the section boundary.

ZMX

Maximum Z coordinate of the section boundary.

YS

Distance from GC of the section to Y top fiber.

ZS

Distance from GC of the section to Z top fiber.

YM

Distance from GC to center of shear forces M in Y.

ZM

Distance from GC to center of shear forces M in Z.

IW

Torsional warping modulus.

IYZ

Inertia product.

YWS

Y shear area.

ZWS

Z shear area.

XWT

Torsional modulus.

IUU

U axis bending inertia.

IVV

V axis bending inertia.

IU

U axis radius of gyration.

IV

V axis radius of gyration.

ALP

Angle between main inertia axes and section axes.

V1

Distance to the extreme fiber from U (for L sections).

V2

Distance to the extreme fiber from U (for L sections).

U1

Distance to the extreme fiber from V (for L sections).

U2

Distance to the extreme fiber from V (for L sections).

U3

Distance to the extreme fiber from V (for L sections).

 

Lab1= STRPROP

~CFGET, Par, SECTION, ENTNUM, STRPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to structural properties of cross sections. Valid labels are:

Lab2

Description

ASEC

Type of section used for calculation of structural properties.

1

Gross Generic Section.

2

Steel Gross Section.

3

Steel Net Section.

4

Steel Effective Section.

5

Concrete Gross Section.

6

Concrete Net Section.

7

Concrete Transformed Section.

8

Equivalent Composite Section.

YMN

Minimum Y coordinate of section boundary.

YMX

Maximum Y coordinate of section boundary.

ZMN

Minimum Z coordinate of section boundary.

ZMX

Maximum Z coordinate of section boundary.

TKY

Y thickness.

TKZ

Z thickness.

ARE

Area.

IXX

Torsional inertia.

IYY

Y axis bending inertia.

IZZ

Z axis bending inertia.

YCG

Distance from GC of the section to Y top fiber.

ZCG

Distance from GC of the section to Z top fiber.

YMS

Distance from GC to center of shear forces M in Y.

ZMS

Distance from GC to center of shear forces M in Z.

YWS

Y shear area.

ZWS

Z shear area.

XWT

Torsional modulus.

 

Lab1= EC3PROP

~CFGET, Par, SECTION, ENTNUM, EC3PROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to Eurocode No.3. Valid labels are:

Lab2

Description

AHOLES

Holes area to discount from gross area to obtain net area.

DUCT

Inelastic energy absorption factor.

CHCKTYPE

Type of checking.

 

Lab1= CTESEAPR

~CFGET, Par, SECTION, ENTNUM, CTESEAPR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to CTE DB SE-A code. Valid labels are:

Lab2

Description

AHOLES

Holes area to discount from gross area to obtain net area.

CHCKTYPE

Type of checking.

 

Lab1= EAPROP

~CFGET, Par, SECTION, ENTNUM, EAPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the Spanish code EA. Valid labels are:

Lab2

Description

AHOLES

Hole’s area to discount from gross area to obtain net area.

F

Summation of forces transmitted by bolts in net section.

 

Lab1= LRFDPROP

~CFGET, Par, SECTION, ENTNUM, LRFDPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the LRFD. Valid labels are:

Lab2

Description

AHOLES

Hole’s area to discount from gross area to obtain net area.

 

Lab1= GB50017P

~CFGET, Par, SECTION, ENTNUM, GB50017P, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the GB50017. Valid labels are:

Lab2

Description

AHOLES

Hole’s area to discount from gross area to obtain net area.

RTB

Factor n1/n:

n1

Number of bolts at the calculated section.

n

Number of high strength frictional bolts.

 

Lab1= BS5950PR

~CFGET, Par, SECTION, ENTNUM, BS5950PR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the British Standard 5950. Valid labels are:

Lab2

Description

AHOLES

Hole’s area to discount from gross area to obtain net area.

FORMED

Indicates if the section is hot or cold formed:

0

Cold formed.

1

Hot formed.

 

Lab1= ASMENFPR

~CFGET, Par, SECTION, ENTNUM, ASMENFPR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the ASME BPVC III Subsection NF. Valid labels are:

Lab2

Description

AHOLES

Hole’s area to discount from gross area to obtain net area.

CT

Reduction coefficient in computing effective net area of an axially loaded tension member.

 

Lab1= ASDPROP

~CFGET, Par, SECTION, ENTNUM, ASDPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the AISC-ASD 9th Edition code. Valid labels are:

Lab2

Description

AHOLES

Hole’s area to discount from gross area to obtain net area.

 

Lab1= ASD13PR

~CFGET, Par, SECTION, ENTNUM, ASD13PR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the AISC 13th Edition code. Valid labels are:

Lab2

Description

AHOLES

Hole’s area to discount from gross area to obtain net area.

 

Lab1= N690PROP

~CFGET, Par, SECTION, ENTNUM, N690PROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the ANSI/AISC N690 code. Valid labels are:

Lab2

Description

AHOLES

Hole’s area to discount from gross area to obtain net area.

DUCT

Inelastic energy absorption factor.

 

Lab1= EC2PROP

~CFGET, Par, SECTION, ENTNUM, EC2PROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to Eurocode No.2. Valid labels are

For shear and torsion calculations:

Lab2

Description

DUCT_BN            

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

DUCT_SH

Inelastic energy absorption factor for shear. Used to consider ductility in HCLPF check.

DUCT_TO

Inelastic energy absorption factor for torsion. Used to consider ductility in HCLPF check.

BW_VY

VY minimum depth width.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

RHO1

Longitudinal tension reinforcement ratio.

T

Equivalent wall thickness.

AK

Area enclosed by the center line of thin wall.

UK

Perimeter of AK area.

KEYAST

Situation of torsional reinforcement.

THETA

Angle of concrete compressive struts.

REC

Mechanical cover for properties calculation.

 

For cracking calculations:

 Lab2

Description

FI

Reinforcement bars size for the indicated fiber in IDX1

RHOR

Effective reinforcement ratio for the indicated fiber in IDX1

The valid values for IDX1 are:

1

Y top fiber.

2

Y bottom fiber.

3

Z top fiber.

4

Z bottom fiber.

      

Lab1= ACIPROP

~CFGET, Par, SECTION, ENTNUM, ACIPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the ACI 318 code. Valid labels are:

For shear and torsion calculus:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

BW_VY

VY minimum depth width.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

ACP

Area enclosed by the exterior perimeter of the section.

PCP

External perimeter of concrete section.

AOH

Area enclosed by torsional stirrups.

PH

Perimeter enclosed by torsional stirrups.

AO

Gross area enclosed by the flux of tangential stresses.

TKMIN

Minimum wall thickness.

REC

Mechanical cover for properties calculation.

 

For cracking calculus:

Lab2

Description

CC

Geometrical cover in the indicated fiber in IDX1.

Valid values for IDX1 are:

1

Y top fiber.

2

Y bottom fiber.

3

Z top fiber.

4

Z bottom fiber.

 

Lab1= ACI349PR

~CFGET, Par, SECTION, ENTNUM, ACI349PR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the ACI 349 code. Valid labels are:

For shear and torsion calculus:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

DUCT_SH

Inelastic energy absorption factor for shear. Used to consider ductility in HCLPF check.

DUCT_TO

Inelastic energy absorption factor for torsion. Used to consider ductility in HCLPF check.

REC

Cover for properties calculation. If this data is modified all properties are automatically recalculated.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

ACP

Area enclosed by the exterior perimeter of the section.

PCP

External perimeter of concrete section.

AOH

Area enclosed by torsional stirrups.

PH

Perimeter enclosed by torsional stirrups.

AO

Gross area enclosed by the flux of tangential stresses.

TKMIN

Minimum wall thickness.

REC

Mechanical cover for properties calculation.

 

For cracking calculus:

Lab2

Description

CC

Geometrical cover in the indicated fiber in IDX1.

Valid values for IDX1 are:

1

Y top fiber.

2

Y bottom fiber.

3

Z top fiber.

4

Z bottom fiber.

 

Lab1= EHEPROP

~CFGET, Par, SECTION, ENTNUM, EHEPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to Spanish code EHE. Valid labels are:

For shear and torsion calculus:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

BW_VY

VY minimum depth width.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

RHO1

Longitudinal tension reinforcement amount.

HE

Effective thickness

AE

Area enclosed by the center line of the effective section.

UE

Perimeter of AE area.

KEYAST

Situation of torsional reinforcement.

THETA

Angle of concrete’s compressive struts..

REC

Mechanical cover for properties calculation.

 

For Cracking calculus:

Lab2

Description

FI

Diameter of the thicker tension bar in the indicated fiber in IDX1

RHOr

Effective reinforcement ratio, As/Ac,eff, in the fiber indicated in IDX1

C

Concrete cover in the indicated fiber in IDX1.

S

Distance between longitudinal bars in the fiber indicated in IDX1 The permissible values of IDX1 are:

1

Y top fiber.

2

Y bottom fiber.

3

Z top fiber.

4

Z bottom fiber.

 

Lab1= BS8110PR

~CFGET, Par, SECTION, ENTNUM, BS8110PR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to British Standard 8110. Valid labels are:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

BW_VY

Breadth of section for shear in Y.

BW_VZ

Breadth of section for shear in Z.

D_Y

Effective depth in Y.

D_Z

Effective depth in Z.

AS

Longitudinal tension reinforcement.

Xw

Torsion modulus.

X1

Smaller distance between legs of torsion stirrups.

Y1

Larger distance between legs of torsion stirrups.

REC

Cover for properties’ calculation. If this date is modified all properties are automatically recalculated.

 

Lab1= AS3600PR

~CFGET, Par, SECTION, ENTNUM, AS3600PR, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to Australian Standard 3600. Valid labels are:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

REC

Cover for properties’ calculation. If this date is modified all properties are automatically recalculated.

BW_VY

Breadth of section for shear in Y.

BW_VZ

Breadth of section for shear in Z.

DO_Y

Effective depth in Y.

DO_Z

Effective depth in Z.

THETA

Angle of compression struts.

AST

Area of flexural reinforcement in tension.

AT

Area enclosed by centerline of the outermost closed transverse torsional reinforcement.

UT

Perimeter of centerline of outermost closed transverse torsional reinforcement.

JT

Torsional modulus.

 

Lab1= GB50010

~CFGET, Par, SECTION, ENTNUM, GB50010, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to Chinese code. Valid labels are:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

REC

Reinforcement’s cover.

BW_VY

Minimum width of the section over the effective depth for shear in Y (Art. 7.5.1).

BW_VZ

Minimum width of the section over the effective depth for shear in Z (Art. 7.5.1).

D_Y

Effective depth of the section in Y (Art. 7.5.1).

D_Z

Effective depth of the section in Z (Art. 7.5.1).

HW_VY

Effective depth of the web in Y (Art. 7.5.1).

HW_VZ

Effective depth of the web in Z (Art. 7.5.1).

ACOR

The area enclosed within the hoop reinforcements for torsion Ast1 (Art. 7.6.4).

ACOR1

The area enclosed within the hoop reinforcements for torsion Ast1 (Art. 7.6.4) of branch 1(e. x. Flange).

ACOR2

The area enclosed within the hoop reinforcements for torsion Ast1 (Art. 7.6.4) of branch 2(e. x. Flange).

UCOR

The circumference of the Acor area (Art. 7.6.4).

UCOR1

The circumference of the Acor1 area of branch 1 (Art. 7.6.4).

UCOR2

The circumference of the Acor2 area of branch 2 (Art. 7.6.4).

WT

Plastic resistance of torsion moment (Art. 7.6.4).

WT1

Plastic resistance of torsion moment of branch 1 (Art. 7.6.4).

WT2

Plastic resistance of torsion moment of branch 2 (Art. 7.6.4).

ALF

Ratio of the web depth to the web width (Art. 7.6.1).

ALFH

Affected factor of the thickness of web for torsion (Art. 7.6.6).

 

Lab1= NBR6118

~CFGET, Par, SECTION, ENTNUM, NBR6118, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to Brazilian code NBR6118. Valid labels are:

For shear and torsion calculus:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

BW_VY

VY minimum depth width.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

HE

Effective thickness

AE

Area enclosed by the center line of the effective section.

UE

Perimeter of AE area.

THETA

Angle of concrete’s compressive struts..

REC

Mechanical cover for properties calculation.

 

Lab1= AASHTOHB

~CFGET, Par, SECTION, ENTNUM, AASHTOHB, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the AASHTO Standard Specification for Highway Bridges. Valid labels are:

For shear and torsion calculus:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

BW_VY

VY minimum depth width.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

ACP

Area enclosed by the exterior perimeter of the section.

PCP

External perimeter of concrete section.

AOH

Area enclosed by torsional stirrups.

PH

Perimeter enclosed by torsional stirrups.

AO

Gross area enclosed by the flux of tangential stresses.

TKMIN

Minimum wall thickness.

REC

Mechanical cover for properties calculation.

 

Lab1= IS456P

~CFGET, Par, SECTION, ENTNUM, IS456P, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to Indian Standard 456. Valid labels are

For shear and torsion calculations:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

BW_VY

VY minimum depth width.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

RHO1

Longitudinal tension reinforcement ratio.

Y1

Centre-to-centre distance between corner bars in the Y direction.

Z1

Centre-to-centre distance between corner bars in the Z direction.

REC

Mechanical cover for properties calculation.

 

Lab1= SP52101P

~CFGET, Par, SECTION, ENTNUM, SP52101P, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the Russian code CP 52-101-03. Valid labels are

For shear and torsion calculations:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

BW_VY

VY minimum depth width.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

REC

Mechanical cover for properties calculation.

 

Lab1= SP63133P

~CFGET, Par, SECTION, ENTNUM, SP63133P, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to the Russian code CP 63.13330.2012. Valid labels are

For shear and torsion calculations:

Lab2

Description

DUCT_BN

Inelastic energy absorption factor for bending. Used to consider ductility in HCLPF check.

BW_VY

VY minimum depth width.

BW_VZ

VZ minimum depth width.

D_Y

Effective depth in Y direction.

D_Z

Effective depth in Z direction.

REC

Mechanical cover for properties calculation.

 

Lab1= STEEPROP

~CFGET, Par, SECTION, ENTNUM, STEEPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to steel rolled sections. Valid labels are:

Lab2

Description

IDX1

CivilFEM index of the data set (see CivilFEM Theory Manual for information regarding the different indexes).

IDX2

CivilFEM index of the section among its data set.

 

Lab1= CONCPROP

~CFGET, Par, SECTION, ENTNUM, CONCPROP, Lab2, , IDX1, IDX2, IDX3

Retrieves data referred to concrete sections. Valid labels are:

Lab2

Description

ROG

Geometric amount of bending reinforcement.

ROM

Amount of bending reinforcement in mass.

 

·         ~CFGET – SHLVERT (ENTNUM = Number of shell vertex)

~CFGET, Par, SHLVERT, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= RF16

~CFGET, Par, SHLVERT, ENTNUM, RF16, , , IDX1, IDX2, IDX3

Reference of shell vertex (16 characters). IDX1 indicates the group of 8 characters to retrieve.

IDX1

Group of characters

1

1 to 8

2

9 to 16

 

Lab1= NAME

~CFGET, Par, SHLVERT, ENTNUM, NAME, , , IDX1, IDX2, IDX3

Name assigned to the shell vertex (32 characters). IDX1 indicates the group of 8 characters to retrieve.

IDX1

Group of characters

1

1 to 8

2

9 to 16

3

17 to 24

4

25 to 32

 

Lab1= STP

~CFGET, Par, SHLVERT, ENTNUM, STP, , , IDX1, IDX2, IDX3

Type of shell vertex:

0

Generic.

1

Reinforced concrete.

 

Lab1= THK

~CFGET, Par, SHLVERT, ENTNUM, THK, , , IDX1, IDX2, IDX3

Shell vertex thickness.

 

Lab1= MAT

~CFGET, Par, SHLVERT, ENTNUM, MAT, , , IDX1, IDX2, IDX3

Number of material of shell vertex.

 

Lab1= MTP

~CFGET, Par, SHLVERT, ENTNUM, MTP, , , IDX1, IDX2, IDX3

Type of material of shell vertex:

0

Generic.

2

Concrete.

 

Lab1= REINF

~CFGET, Par, SHLVERT, ENTNUM, REINF, Lab2, , IDX1, IDX2, IDX3

Retrieves properties referred to shell vertices reinforcement. Valid labels are:

Lab2

Description

MAT

Material associated to the vertex shell reinforcement.

MC

Mechanical cover of shell vertex.

ASSXT

Area per unit length of reinforcement in X top face.

ASSXB

Area per unit length of reinforcement in X bottom face.

ASSYT

Area per unit length of reinforcement in Y top face.

ASSYB

Area per unit length of reinforcement in Y bottom face.

SXT

Separation between bars in X top face

SXB

Separation between bars in X bottom face

SYT

separation between bars in Y top face

SYB

separation between bars in Y bottom face

PHIXT

Diameter of X top bars

PHIXB

Diameter of X bottom bars

PHIYT

Diameter of Y top bars

PHIYB

Diameter of Y bottom bars

KRNF

Situation of reinforcements

0

Non braced bars.

1

Braced bars.

ALP

Angle between the reinforcement and the local Y axis of the element (Wood method).

 

Lab1= IPREINF

~CFGET, Par, SHLVERT, ENTNUM, IPREINF, Lab2, , IDX1, IDX2, IDX3

Lab2

Descripción

MATIP

Material associated to the vertex shell in plane shear reinforcement.

ASSIPX

Area per unit area of in plane shear reinforcement in the X direction.

ASSIPY

Area per unit area of in plane shear reinforcement in the Y direction.

Lab1= SHREINF

~CFGET, Par, SHLVERT, ENTNUM, SHREINF, Lab2, , IDX1, IDX2, IDX3

Retrieves properties referred to shell vertices shear reinforcement. Valid labels are:

Lab2

Description

MATOP

Material associated to the vertex shell shear reinforcement.

ASSOP

Area per unit area of shear reinforcement.

PHIOP

Bar diameters (in milimetres).

NXOP

Number of bars per unit length in the X direction.

NYOP

Number of bars per unit length in the Y direction.

SXOP

Distance between bars in the X direction.

SYOP

ASSOPX

ASSOPY

Distance between bars in the Y direction.

Area per unit area of shear reinforcement in the X direction.

Area per unit area of shear reinforcement in the Y direction.

 

Lab1= CP

~CFGET, Par, SHLVERT, ENTNUM, CP, Lab2, , IDX1, IDX2, IDX3

Retrieves code properties of shell vertex. Valid labels are:

Lab2

Description

THETA

Angle of the concrete compressive strut with the direction of reinforcement.

DUCT_BN_X

Inelastic energy absorption factor for bending in X direction. Used to consider ductility in HCLPF check.

DUCT_BN_Y

Inelastic energy absorption factor for bending in Y direction. Used to consider ductility in HCLPF check.

DUCT_OP_X

Inelastic energy absorption factor for out of plane shear in X direction. Used to consider ductility in HCLPF check.

DUCT_OP_Y

Inelastic energy absorption factor for out of plane shear in Y direction. Used to consider ductility in HCLPF check.

DUCT_IP_X

Inelastic energy absorption factor for in plane shear in X direction. Used to consider ductility in HCLPF check.

DUCT_IP_Y

Inelastic energy absorption factor for in plane shear in Y direction. Used to consider ductility in HCLPF check.

 

 

·         ~CFGET – MEMBPROP (ENTNUM = Number of member property)

 

~CFGET, Par, MEMBPROP, EntNum, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= RF16

~CFGET, Par, MEMBPROP, EntNum, RF16, , , IDX1, IDX2, IDX3

Reference of member property (16 characters). Indicates the group of 8 characters to retrieve.

 

IDX1

Group of characters

1

1 to 8

2

9 to 16

 

Lab1= NAME

~CFGET, Par, MEMBPROP, EntNum, NAME, , , IDX1, IDX2, IDX3

Number of member property (32 characters). Indicates the group of 8 characters to retrieve.

IDX1

Group of characters

1

1 to 8

2

9 to 16

3

17 to 24

4

25 to 32

 

Lab1= EC3                                                                              

~CFGET, Par, MEMBPROP, EntNum, EC3, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for Eurocode No 3 checking. Valid labels are:

Lab2

Description

L

Length between between lateral restrains.

K

Lateral buckling k factor.

KW

Lateral buckling kw factor.

C1

Lateral buckling C1 factor.

C2

Lateral buckling C2 factor.

C3

Lateral buckling C3 factor.

BETAMY

Equivalent uniform movement factor.

BETAMZ

Equivalent uniform movement factor.

BETAMLT

Equivalent uniform movement factor.

PSIVEC

Reduction factor for vectorial effects.

LATBUCK

Susceptible to lateral-torsional buckling

0

Yes

1

No

CFBUCKXY

xy plane buckling factor (Mz in CivilFEM axis).

CFBUCKXZ

xz plane buckling factor (My in CivilFEM axis).

CHCKAXIS

 CivilFEM axis that is “Y” axis of Eurocode No.3.

0

Not defined

1

CivilFEM “-Z”

2

CivilFEM “+Y”

3

CivilFEM “+Z”

4

CivilFEM “-Y”

 

Lab1= CTESEA                                                                      

~CFGET, Par, MEMBPROP, EntNum, CTESEA, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for CTE DB SE-A code checking. Valid labels are:

Lab2

Description

L

Length between between lateral restrains.

K

Lateral buckling k factor.

KW

Lateral buckling kw factor.

C1

Lateral buckling C1 factor.

CMY

Equivalent uniform movement factor.

CMZ

Equivalent uniform movement factor.

CMLT

Equivalent uniform movement factor.

PSIVEC

Reduction factor for vectorial effects.

LATBUCK

Susceptible to lateral-torsional buckling

0

Yes

1

No

CFBUCKXY

xy plane buckling factor (Mz in CivilFEM axis).

CFBUCKXZ

xz plane buckling factor (My in CivilFEM axis).

CHCKAXIS

 CivilFEM axis that is “Y” axis of CTESEA.

0

Not defined

1

CivilFEM “-Z”

2

CivilFEM “+Y”

3

CivilFEM “+Z”

4

CivilFEM “-Y”

 

Lab1= EA

~CFGET, Par, MEMBPROP, EntNum, EA, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for EA checking. Valid labels are:

Lab2

Description

MEMBTYPE

Member type

1

Beam

2

Column

L

Unbraced length of member.

BETAXY

Buckling factor on xy (Mz) plane.

BETAXZ

Buckling factor on xz (My) plane.

 

Lab1= LRFD                                                                           

~CFGET, Par, MEMBPROP, EntNum, LRFD, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for LRFD (second edition) checking. Valid labels are:

Lab2

Description

L

Length between restraints (B3).

KY

Buckling factor Y axis (B7).

KZ

Buckling factor Z axis (B7).

KTOR

Length factor for torsional buckling (App.E3).

CB

Bending coefficient dependent on moment gradient (F1.2a).

LB

Laterally unbraced length (F1.2).

 

Lab1= LRFD13                                                                       

~CFGET, Par, MEMBPROP, EntNum, LRFD13, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for LRFD (13th edition) checking. Valid labels are:

Lab2

Description

L

Length between restraints.

KY

Buckling factor Y axis (C1.2).

KZ

Buckling factor Z axis (C1.2).

KTOR

Length factor for torsional buckling (E4).

CB

Lateral-torsional buckling factor for nonuniform moment diagrams when both ends are braced (F1).

LB

Laterally unbraced length (E2).

 

Lab1= GB50017                                                                     

~CFGET, Par, MEMBPROP, EntNum, GB50017, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for GB50017 checking. Valid labels are:

Lab2

Description

GAMMAY

Plastic developing coefficient for Y axis.

GAMMAZ

Plastic developing coefficient for Z axis.

TSECY

Section type for Y axis.

TSECZ

Section type for Z axis.

L

Unbraced length of member.

KY

Buckling factor on Y axis.

KZ

Buckling factor on Z axis.

 

Lab1= AASHTO10                                                                 

~CFGET, Par, MEMBPROP, EntNum, AASHTO10, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for AASHTO LRFD BRIDGE 2010 checking. Valid labels are:

Lab2

Description

L

Length between restraints.

KY

Buckling factor Y axis .

KZ

Buckling factor Z axis.

KTOR

Length factor for torsional buckling.

CB

Lateral-torsional buckling factor for nonuniform moment diagrams when both ends are braced.

LB

Laterally unbraced length.

RP

U

LV

Reduction factor for holes.

Shear Lag factor.

Distance between points of maximum and zero shear.

 

Lab1= IS800                                                                            

~CFGET, Par, MEMBPROP, EntNum, IS800, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for Indian Standard 800 (2007) checking. Valid labels are:

Lab2

Description

L

Length between between lateral restrains.

K

Lateral buckling k factor.

KW

Lateral buckling kw factor.

C1

Lateral buckling C1 factor.

C2

Lateral buckling C2 factor.

C3

Lateral buckling C3 factor.

BETAMY

Equivalent uniform movement factor.

BETAMZ

Equivalent uniform movement factor.

BETAMLT

Equivalent uniform movement factor.

PSIVEC

Reduction factor for vectorial effects.

LATBUCK

Susceptible to lateral-torsional buckling

0

Yes

1

No

CFBUCKXY

xy plane buckling factor (Mz in CivilFEM axis).

CFBUCKXZ

xz plane buckling factor (My in CivilFEM axis).

CHCKAXIS

 CivilFEM axis that is “Y” axis of Indian Standard 800 (2007).

0

Not defined

1

CivilFEM “-Z”

2

CivilFEM “+Y”

3

CivilFEM “+Z”

4

CivilFEM “-Y”

 

Lab1= BS5950                                                                        

~CFGET, Par, MEMBPROP, EntNum, BS5950, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for British Standard 5950 (1985 or 2001) valid labels are:

Lab2

Description

L

Length between restraints.

KLtx

Lateral buckling factor K for X axis

KLty

Lateral buckling factor K for Y axis

KCX

Coefficient for compression buckling X axis

KCY

Coefficient for compression buckling Y axis

CteRob

Robertson constant.

n

Slenderness correction factor.

m

Equivalent uniform moment factor

DL

Depth of flange’s stiffeners

CHCKAXIS

CivilFEM axis that is “X” axis of BS5950.

0

Not defined

1

CivilFEM “-Z”

2

CivilFEM “+Y”

3

CivilFEM “+Z”

4

CivilFEM “-Y”

CFBUCKX

Buckling factor in plane ZX (Mz in CivilFEM axes).

CFBUCKY

Buckling factor in plane ZY (My in CivilFEM axes).

D/a

Intermediate stiffeners depth.

mx

Equivalent uniform moment factor for major axis flexural bending

my

Equivalent uniform moment factor for minor axis flexural bending

mlt

Equivalent uniform moment factor for lateral torsional buckling

 

Lab1= GB50010                                                                                       

~CFGET, Par, MEMBPROP, EntNum, GB50010, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for Chinese code. The valid labels are:

Lab2

Description

MEMBTYPE

Member type:

1

Beam.

2

Column.

3

Bracing column for frame-wall structures.

4

Wall.

5

Link beam of walls.

MEMBLOAD

Load type:

1

FORCE. The effect of concentrated force exceeds 75% in independent beam.

2

FRAME. The member comes from frame structure.

0

OTHER. Not “Frame” or “Force”.

 

Lab1= ASME_NF                                                                   

~CFGET, Par, MEMBPROP, EntNum, ASME_NF, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for checking according to ASME BPVC III Subsection NF. Valid labels are:

Lab2

Description

L

Length between restraints.

KY

Buckling factor Y axis.

KZ

Buckling factor Z axis.

CBY

Bending coefficient dependent on moment gradient on Y axis (NF-3322.1).

CBZ

Bending coefficient dependent on moment gradient on Z axis (NF-3322.1).

CMY

Coefficient applied to bending term in interaction equation and dependent upon column curvature caused by applied moments on Y axis (NF-3322.1).

CMZ

Coefficient applied to bending term in interaction equation and dependent upon column curvature caused by applied moments on Z axis (NF-3322.1).

PIN

Pin-connected:

0

No.

1

Yes.

COLUMN

Member type:

0

Not a column.

1

Column.

BRACED

Braced:

0

No.

1

Yes.

 

Lab1= ASD9                                                                            

~CFGET, Par, MEMBPROP, EntNum, ASD9, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for chacking according to AISC-ASD Ninth Edition. Valid labels are:

Lab2

Description

L

Length between restraints (B.3).

KXY

Buckling factor in XY plane (table C-C2.1).

KXZ

Buckling factor in XZ plane (table C-C2.1).

CB

Bending coefficient dependent on moment gradient (F1.3).

KZ

Effective length factor for torsional buckling (table C-C2.1).

 

Lab1= ASD13                                                                         

~CFGET, Par, MEMBPROP, EntNum, ASD13, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for chacking according to AISC-ASD 13th Edition. Valid labels are:

Lab2

Description

L

Length between restraints.

KXY

Buckling factor in XY plane (table C-C2.2).

KXZ

Buckling factor in XZ plane (table C-C2.2).

CB

Bending coefficient dependent on moment gradient (F1.1).

KZ

Effective length factor for torsional buckling (table C-C2.2).

 

Lab1= AISC14                                                                        

~CFGET, Par, MEMBPROP, EntNum, AISC14, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for chacking according to AISC-ASD 14th Edition. Valid labels are:

Lab2

Description

L

Laterally unbraced length of member (E2).

LB

Length between points that are either braced against lateral displacement of compression flange (F2.2).

KXY

Buckling factor in XY plane (E4).

KXZ

Buckling factor in XZ plane (E4).

CB

Lateral-torsional buckling modification factor for nonuniform moment diagrams (F1).

KTOR

Effective length factor for torsional buckling (E4).

 

Lab1= AISC15        

~CFGET, Par, MEMBPROP, EntNum, AISC15, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for chacking according to AISC-ASD 15th Edition. Valid labels are:

Lab2

Description

L

Laterally unbraced length of member (E2).

LB

Length between points that are either braced against lateral displacement of compression flange (F2.2).

KXY

Buckling factor in XY plane (E4).

KXZ

Buckling factor in XZ plane (E4).

CB

Lateral-torsional buckling modification factor for nonuniform moment diagrams (F1).

KTOR

Effective length factor for torsional buckling (E4).

 

Lab1= N690_94                                                                      

~CFGET, Par, MEMBPROP, EntNum, N690_94, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for chacking according to ANSI/AISC N690-1994. Valid labels are:

Lab2

Description

L

Length between restraints.

KXY

Buckling factor in XY plane (table CQ1.8.1).

KXZ

Buckling factor in XZ plane (table CQ1.8.1).

CB

Bending coefficient dependent on moment gradient (Q1.5.1.4.5).

KZ

Effective length factor for torsional buckling (CQ1.5.1.3.6).

CMY

Coefficient for compression members dependent on joint translation in plane XY (Q1.6.1)

CMZ

Coefficient for compression members dependent on joint translation in plane XZ (Q1.6.1)

 

Lab1= N690_06                                                                      

~CFGET, Par, MEMBPROP, EntNum, N690_06, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties needed for chacking according to ANSI/AISC N690-06. Valid labels are:

Lab2

Description

L

Length between restraints.

KXY

Buckling factor in XY plane (table NC-C2.2).

KXZ

Buckling factor in XZ plane (table NC-C2.2).

CB

Bending coefficient dependent on moment gradient (NF1-1).

KZ

Effective length factor for torsional buckling (table NC-C2.2).

LB

Flexural length between restraints (NF2.2).

 

Lab1= NLC

~CFGET, Par, MEMBPROP, EntNum, NLC, Lab2, , IDX1, IDX2, IDX3

Only for Bridges and Civil Non Linearities module. The valid labels are:

Lab2

Description

KEYNL

Member behavior

0

Linear

1

Non Linear

 

Lab1= ACI318

~CFGET, Par, MEMBPROP, EntNum, ACI318, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties for the ACI 318 code. Valid labels are:

Lab2

Description

PHI

Strength reduction factor for axial+bending.

 

Lab1= ACI349

~CFGET, Par, MEMBPROP, EntNum, ACI349, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties for the ACI 349 code. Valid labels are:

Lab2

Description

PHI

Strength reduction factor for axial+bending.

 

Lab1= AS3600

~CFGET, Par, MEMBPROP, EntNum, AS3600, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties for the Australian AS3600 code. Valid labels are:

Lab2

Description

PHI

Strength reduction factor for axial+bending.

 

Lab1= AASHTOHB

~CFGET, Par, MEMBPROP, EntNum, AS3600, Lab2, , IDX1, IDX2, IDX3

Retrieves member properties for the AASHTO Standard Specifications for Highway Bridges. Valid labels are:

Lab2

Description

PHI

Strength reduction factor for axial+bending.

 

 

·         ~CFGET – BMSHPROP (ENTNUM = Number of beam or shell property)

 

~CFGET, Par, BMSHPROP, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= RF16

~CFGET, Par, BMSHPROP, ENTNUM, RF16, , , IDX1, IDX2, IDX3

Reference of beam or shell property (16 characters). Indicates the group of 8 characters to retrieve.

IDX1

Character group

1

1 to 8

2

9 to 16

 

Lab1= NAME

~CFGET, Par, BMSHPROP, ENTNUM, NAME, , , IDX1, IDX2, IDX3

Name assigned to beam or shell property (32 characters). Indicates the group of 8 characters to retrieve.

IDX1

Character group

1

1 to 8

2

9 to 16

3

17 to 24

4

25 to 32

 

Lab1= TYP

~CFGET, Par, BMSHPROP, ENTNUM, TYP, , , IDX1, IDX2, IDX3

Type of beam or shell property: 1- Beam, 2-Shell.

 

Lab1= NSEC

~CFGET, Par, BMSHPROP, ENTNUM, NSEC, , , IDX1, IDX2, IDX3

Number of cross sections (if TYP=1) or shell vertex (if TYP=2) which form the beam or shell.

 

Lab1= USEC

~CFGET, Par, BMSHPROP, ENTNUM, USEC, , , IDX1, IDX2, IDX3

Numbering of cross sections or shell vertices that form (I, J, K, L) vertices of shells or beams properties. In IDX1 (IDX1£ 4) the beam or shell vertex for which the data is going to be retrieve must be specified.

 

Lab1= KEYOFF

~CFGET, Par, BMSHPROP, ENTNUM, KEYOFF, , , IDX1, IDX2, IDX3

OFFSET of cross sections:

0     Node at the center of gravity.

1     Node at the origin of the coordinates system of the section.

2     Node location defined by the user.

3    Node at the shear center

 

Lab1= ROUT

~CFGET, Par, BMSHPROP, ENTNUM, ROUT, , , IDX1, IDX2, IDX3

Element type for which ANSYS real constants are defined.

 

Lab1= UMPR

~CFGET, Par, BMSHPROP, ENTNUM, UMPR, , , IDX1, IDX2, IDX3

Number of corresponding member property.

 

Lab1= RC

~CFGET, Par, BMSHPROP, ENTNUM, RC, , , IDX1, IDX2, IDX3

Value of ANSYS real constant at the position IDX1.

 

Lab1= OSYI

~CFGET, Par, BMSHPROP, ENTNUM, OSYI, , , IDX1, IDX2, IDX3

Node location of section I. Y coordinate referred to section axis.

 

Lab1= OSZI

~CFGET, Par, BMSHPROP, ENTNUM, OSZI, , , IDX1, IDX2, IDX3

Node location of section I. Z coordinate referred to section axis.

 

Lab1= OSYJ

~CFGET, Par, BMSHPROP, ENTNUM, OSYJ, , , IDX1, IDX2, IDX3

Node location of section J. Y coordinate referred to section axis.

 

Lab1= OSZJ

~CFGET, Par, BMSHPROP, ENTNUM, OSZJ, , , IDX1, IDX2, IDX3

Node location of section J. Z coordinate referred to section axis.

 

·         ~CFGET – SLDSEC (ENTNUM = Number of solid section)

~CFGET, Par, SLDSEC, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= RF16

~CFGET, Par, SLDSEC, ENTNUM, RF16, , , IDX1, IDX2, IDX3

Reference to solid section (16 characters). Indicates the group of 8 characters to retrieve.

IDX1

Group of characters

1

1 to 8

2

9 to 16

 

Lab1= NAME

~CFGET, Par, SLDSEC, ENTNUM, NAME, , , IDX1, IDX2, IDX3

Name assigned to solid section (32 characters). Indicates the group of 8 characters to retrieve.

IDX1

Group of characters

1

1 to 8

2

9 to 16

3

17 to 24

4

25 to 32

 

Lab1= UMPR

~CFGET, Par, SLDSEC, ENTNUM, UMPR, , , IDX1, IDX2, IDX3

Number of member property associated to solid section.

 

·         ~CFGET – ELEMENT (ENTNUM = Element number)

~CFGET, Par, ELEMENT, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= ICS

~CFGET, Par, ELEMENT, ENTNUM, ICS,, Lab2, , IDX1, IDX2, IDX3

Transverse section associated to element ENTNUM at end Lab2.

Lab2

Description

I

End I

J

End J

 

Lab1= IVTX

~CFGET, Par, ELEMENT, ENTNUM, IVTX,, Lab2, , IDX1, IDX2, IDX3

Shell vertex associated to element ENTNUM at end Lab2.

Lab2

Description

I

End I

J

End J

K

End K

L

End L

 

Lab1= IMP

~CFGET, Par, ELEMENT, ENTNUM, IMP,, Lab2, , IDX1, IDX2, IDX3

Member property associated to element ENTNUM at end Lab2.

Lab2

Description

I

End I

J

End J

 

Lab1= IBP

~CFGET, Par, ELEMENT, ENTNUM, IBP,, Lab2, , IDX1, IDX2, IDX3

Beam property associated to element ENTNUM at end Lab2.

Lab2

Description

I

End I

J

End J

 

Lab1= FORCE

~CFGET, Par, ELEMENT, ENTNUM, FORCE, Lab2, Lab3, IDX1, IDX2, IDX3

Forces and moments at element ENTNUM at the element end specified in Lab3. If it is a beam element:

Lab2

Description

FX

Axial force

FY

Shear force Y

FZ

Shear force Z

MX

Torsional moment

MY

Bending moment Y

MZ

Bending moment Z

IFX

Isostatic Axial force

IFY

Isostatic Shear force in Y

IFZ

Isostatic Shear force in Z

IMX

Isostatic Torsional moment

IMY

Isostatic Bending moment Y

IMZ

Isostatic Bending moment Z

HFX

Hyperstatic Axial force

HFY

Hyperstatic Shear force in Y

HFZ

Hyperstatic Shear force in Z

HMX

Hyperstatic Torsional moment

HMY

Hyperstatic Bending moment Y

HMZ

Hyperstatic Bending moment Z

 

If it is a shell element:

Lab2

Description

TX

Axial force in X direction

TY

Axial force in Y direction

TXY

Shear force in XY plane

NX

Shear force in X

NY

Shear force in Y

MX

Bending moment on X

MY

Bending moment on Y

MXY

Torsional moment XY

 

For both types of elements

Lab3

Description

I

End I

J

End J

K

End K

L

End L

 

Lab1= STRESS

~CFGET, Par, ELEMENT, ENTNUM, STRESS, Lab2, Lab3, IDX1, IDX2, IDX3

Stresses at element ENTNUM at end Lab3 in point IDX1. In the case of maximum, minimum or maximum in absolute value, field IDX1 will be ignored.

Lab2

Stress component

SX

Stress SX.

SY

Stress SY.

SZ

Stress SZ.

SXY

Stress SXY.

SYZ

Stress SYZ.

SXZ

Stress

SX_MIN

Minimum stress SX

SY_MIN

Minimum stress SY

SZ_MIN

Minimum stress SZ

SXY_MIN

Minimum stress SXY

SYZ_MIN

Minimum stress SYZ

SXZ_MIN

Minimum stress SXZ

SX_MAX

Maximum stress SX

SY_MAX

Maximum stress SY

SZ_MAX

Maximum stress SZ

SXY_MAX

Maximum stress SXY

SYZ_MAX

Maximum stress SYZ

SXZ_MAX

Maximum stress SXZ

SX_ABS

Maximum stress SX in absolute value

SY_ABS

Maximum stress SY in absolute value

SZ_ABS

Maximum stress SZ in absolute value

SXY_ABS

Maximum stress SXY in absolute value

SYZ_ABS

Maximum stress SYZ in absolute value

SXZ_ABS

Maximum stress SXZ in absolute value

 

The section or vertex from which stresses are obtained are the following:

Lab3

Description

I

End I

J

End J

K

End K

L

End L

 

Lab1= STRAIN

~CFGET, Par, ELEMENT, ENTNUM, STRAIN, Lab2, Lab3, IDX1, IDX2, IDX3

Strains at element ENTNUM at end Lab3 in point IDX1.In the case of maximum, minimum or maximum in absolute value, field IDX1 will be ignored.

Lab2

Strain component

EPSX

Strain ex.

EPSY

Strain ey.

EPSZ

Strain ez.

EPSXY

Strain exy.

EPSYZ

Strain eyz.

EPSXZ

Strain exz.

EPX_MIN

Minimum Strain ex

EPY_MIN

Minimum Strain ey

EPSZ_MIN

Minimum Strain ez

EPXY_MIN

Minimum Strain exy

EPYZ_MIN

Minimum Strain eyz

EPXZ_MIN

Minimum Strain exz

EPX_MAX

Maximum Strain ex

EPY_MAX

Maximum Strain ey

EPZ_MAX

Maximum Strain ez

EPXY_MAX

Maximum Strain exy

EPYZ_MAX

Maximum Strain eyz

EPXZ_MAX

Maximum Strain exz

EPX_ABS

Maximum Strain ex in absolute value

EPY_ABS

Maximum Strain ey in absolute value

EPZ_ABS

Maximum Strain ez in absolute value

EPXY_ABS

Maximum Strain exy in absolute value

EPYZ_ABS

Maximum Strain eyz in absolute value

EPXZ_ABS

Maximum Strain exz in absolute value

 

The cross section or vertex from which stresses are obtained is:

Lab3

Description

I

End I

J

End J

K

End K

L

End L

 

 

Lab1= RESULT

~CFGET, Par, ELEMENT, ENTNUM, RESULT, Lab2, Lab3, IDX1, IDX2, IDX3

Lab2 result for actual alternative (use command ~CFSET to point to the right alternative) at element ENTNUM at end Lab3.

The Lab2 label depends on the selected alternative, being valid those of commands ~PLLSSTL, ~PLLSCON, ~PLSHCON, ~HCLPFCN and ~HCLPFST.

IDX3 value must be set to 1(IDX3=1) when retrieving values from seismic margin check results (~HCLPFCN and ~HCLPFST commands).

Moreover the following results are also available:

For Eurocode 3, effective section parameters:

Lab2

Description

A

Area.

IXX

Torsional inertia.

IYY

Moment of inertia Y axis.

IZZ

Moment of inertia Z axis.

WY

Elastic modulus Y

WZ

Plastic modulus Z

WPY

Plastic modulus Y

WPZ

Plastic modulus Z

IY

Radius of giration Y axis

IZ

Radius of giration Z axis

YG

Center of gravity Y coordinate

ZG

Center of gravity Z coordinate

YMN

Minimum Y of section contour

YMX

Maximum Y of section contour

ZMN

Minimum Z of section contour

ZMX

Maximum Z of section contour

YS

Distance CDG -> YTop Fiber

ZS

Distance CDG -> ZTop Fiber

YM

Distance CDG -> M according to Y axis

ZM

Distance CDG -> M according to Z axis

IW

Warping modulus

IYZ

Product of inertia

YWS

Resistance area to shear in Y direction

ZWS

Resistance area to shear in Z direction

XWT

Torsional modulus

IUU

Moment of inertia according to U axis

IVV

Moment of inertia according to V axis

IU

Radius of gyration according to U axis

IV

Radius of gyration according to V axis

ALP

Angle Y->U or Z->V (Sexag.)

V1

Distance to extreme fiber from U (for L sections).

V2

Distance to extreme fiber from U (for L sections).

U1

Distance to extreme fiber from V (for L sections).

U2

Distance to extreme fiber from V (for L sections).

U3

Distance to extreme fiber from V (for L sections).

 

Steel plates reduction parameters for Eurocode 3:

Lab2

IDX1

Description

CLASS

 

Class

AXIS

 

Bending axis for code checking

PC

Plate Ner

Plate class

PF1

Plate Ner

Plate reduction factor at point 1

PF2

Plate Ner

Plate reduction factor at point 2

 

Steel plates reduction parameters for LRFD:

Lab2

IDX1

Description

CLS_COMP

 

Compression class

CLS_FLEX

 

Bending class

RATIO

Plate Ner

Width to thickness ratio (b/t)

LAMBDP_C

Plate Ner

lP compression

LAMBDR_C

Plate Ner

lR compression

CLASE_C

Plate Ner

Plate Compression class

LAMBDP_F

Plate Ner

lP bending

LAMBDR_F

Plate Ner

lR bending

CLASE_F

Plate Ner

Plate bending class

 

The section or vertex from which stresses are calculated are:

Lab3

Description

I

End I

J

End J

K

End K

L

End L

 

 

·         ~CFGET – SOLID (ENTNUM = Number of SOLID SECTION)

~CFGET, Par, SOLID, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= ICS

~CFGET, Par, SOLID, ENTNUM, ICS, , , IDX1, IDX2, IDX3

Transverse cross section associated to solid section ENTNUM.

 

Lab1= IMP

~CFGET, Par, SOLID, ENTNUM, IMP, , , IDX1, IDX2, IDX3

Member property associated to solid section ENTNUM.

 

Lab1= FORCE

~CFGET, Par, SOLID, ENTNUM, FORCE, Lab2, , IDX1, IDX2, IDX3

Forces at solid section ENTNUM:

Lab2

Description

FX

Axial force

FY

Shear force in Y

FZ

Shear force in Z

MX

Torsional moment

MY

Bending moment Y

MZ

Bending moment Z

IFX

Isostatic Axial force

IFY

Isostatic Shear force in Y

IFZ

Isostatic Shear force in Z

IMX

Isostatic Torsional moment

IMY

Isostatic Bending moment Y

IMZ

Isostatic Bending moment Z

HFX

Hyperstatic Axial force

HFY

Hyperstatic Shear force in Y

HFZ

Hyperstatic Shear force in Z

HMX

Hyperstatic Torsional moment

HMY

Hyperstatic Bending moment Y

HMZ

Hyperstatic Bending moment Z

 

Lab1= STRESS

~CFGET, Par, solid, ENTNUM, STRESS, Lab2, , IDX1, IDX2, IDX3

Stresses at element ENTNUM at end Lab3 in point IDX1. In the case of maximum, minimum or maximum in absolute value, field IDX1 will be ignored.

Lab2

Stress component

SX

Stress SX.

SY

Stress SY.

SZ

Stress SZ.

SXY

Stress SXY.

SYZ

Stress SYZ.

SXZ

Stress SXZ.

SX_MIN

Minimum stress SX

SY_MIN

Minimum stress SY

SZ_MIN

Minimum stress SZ

SXY_MIN

Minimum stress SXY

SYZ_MIN

Minimum stress SYZ

SXZ_MIN

Minimum stress SXZ

SX_MAX

Maximum stress SX

SY_MAX

Maximum stress SY

SZ_MAX

Maximum stress SZ

SXY_MAX

Maximum stress SXY

SYZ_MAX

Maximum stress SYZ

SXZ_MAX

Maximum stress SXZ

SX_ABS

Maximum stress SX in absolute value

SY_ABS

Maximum stress SY in absolute value

SZ_ABS

Maximum stress SZ in absolute value

SXY_ABS

Maximum stress SXY in absolute value

SYZ_ABS

Maximum stress SYZ in absolute value

SXZ_ABS

Maximum stress SXZ in absolute value

 

Lab1= STRAIN

~CFGET, Par, SOLID, ENTNUM, STRAIN, Lab2, , IDX1, IDX2, IDX3

Strains in solid section ENTNUM.

Lab2

Strain component

EPSX

Strain eX.

EPSY

Strain eY.

EPSZ

Strain eZ.

EPSXY

Strain eXY.

EPSYZ

Strain eYZ.

EPSXZ

Strain eXZ.

EPSX_MIN

Minimum strain eX

EPSY_MIN

Minimum strain eY

EPSZ_MIN

Minimum strain eZ

EPSXY_MIN

Minimum strain eXY

EPSYZ_MIN

Minimum strain eYZ

EPSXZ_MIN

Minimum strain eXZ

EPSX_MAX

Maximum strain eX

EPSY_MAX

Maximum strain eY

EPSZ_MAX

Maximum strain eZ

EPSXY_MAX

Maximum strain eXY

EPSYZ_MAX

Maximum strain eYZ

EPSXZ_MAX

Maximum strain eXZ

EPSX_ABS

Maximum strain eX in absolute value

EPSY_ABS

Maximum strain eY in absolute value

EPSZ_ABS

Maximum strain eZ in absolute value

EPSXY_ABS

Maximum strain eXY in absolute value

EPSYZ_ABS

Maximum strain eYZ in absolute value

EPSXZ_ABS

Maximum strain eXZ in absolute value

 

Lab1= RESULT

~CFGET, Par, SOLID, ENTNUM, RESULT, Lab2, , IDX1, IDX2, IDX3

Lab2 result for actual alternative (use command ~CFSET to point to the right alternative) at solid section SOLID.

The Lab2 label depends on the selected alternative, being valid the ones for ~CFGET – ELEMENT.

 

·         ~CFGET – SLOPE (ENTNUM is an empty field)

 

~CFGET, Par, SLOPE, , Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= DATGEN

~CFGET, Par, SLOPE, , DATGEN, Lab2, , IDX1, IDX2, IDX3

Retrieves general data relative to the finite element model that has been exported to the Geotechnical Module of CivilFEM. The data available to retrieve will be introduced in parameter Lab2.

Lab2

Description

NPT

Number of points of the exported model.

NTS

Number of tesellas of the exported model.

NPWP

Number of piezometric lines defined.

MAXPWP

Largest number of piezometric line.

NRE

Number of earth reinforcement groups defined.

SEISMH

Horizontal seismic acceleration.

SEISMV

Vertical seismic acceleration.

MOV

Movement direction of the slip surfaces.

1

Left

2

Right

0

Both

KCN

Coordinate system with which the model was exported.

NPOL

Number of vertical segments introduced by the user to generate polygonals.

NSLICES

Number of slices for each sliding surface.

NITER

Maximum number of iterations.

METHOD

Selected analysis method:

0

Fellenius

1

Bishop

2

Janbu - Simplified

3

Janbu - Modified

10

Finite Element Method

 UMTH

Selected analysis method to calculate the pore water pressure.

1

Traditional

2

Ru

3

Import seepage analysis results

TOL

Tolerance of iterations.

MAXF

Maximum value of screen output.

DATE

Date in which command ~SLPIN was executed.

TIME

Hour in which command ~SLPIN was executed.

 

Lab1= PWP

~CFGET, Par, SLOPE, , PWP, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the pore water pressure. The data available to retrieve will be introduced in parameter Lab2.

Lab2

Description

NEXT

Retrieves the number of the following piezometric line to the one introduced in IDX1.

U

Pressure on line IDX1 (in units of water column).

NPT

Number of points of the piezometric line introduced in IDX1.

X

X coordinate of the point IDX2 which lies in the piezometric line introduced in IDX1.

Y

Y coordinate of the point IDX2 which lies in the piezometric line introduced in IDX1.

 

Lab1= POL

~CFGET, Par, SLOPE, , POL, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the vertical segments which define the polygonal surfaces. The data available to retrieve will be introduced in parameter Lab2.

Lab2

Description

NP

Number of points along the vertical segment introduced in IDX1.

X

X coordinate of the vertical segment introduced in IDX1.

Y

Y coordinate of the vertical segment introduced in IDX1 for the point selected in IDX2 (IDX2 £ NP).

 

Lab1= SURF

~CFGET, Par, SLOPE, , SURF, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the sliding surfaces. The data available to retrieve will be introduced in parameter Lab2.

Lab2

Description

N

Number of sliding surfaces.

NVALID

Number of valid sliding surfaces.

NEXT

Next valid sliding surface to the one expressed in IDX1.

PX

X coordinate of point 0,1 or 2 introduced in IDX1 of the mesh of centers.

PY

Y coordinate of point 0,1 or 2 introduced in IDX1 of the mesh of centers.

N1

Number of divisions on side 0-1 of the mesh of centers.

N2

Number of divisions on side 0-2 of the mesh of centers.

VX

X coordinate of point 1,2,3 or 4 introduced in IDX1 of the mesh of tangents.

VY

Y coordinate of point 1,2,3 or 4 introduced in IDX1 of the mesh of tangents.

NTAN

Number of tangents.

CX

X coordinate of the center of the circle introduced in IDX1.

CY

Y coordinate of the center of the circle introduced in IDX1.

CR

Radius of the circle introduced in IDX1.

VALID

Validity of the circle introduced in IDX1. If valid, a value of 1 will be returned.

NPSURF

Number of points of the sliding surface introduced in IDX1.

XSURF

X coordinate of the point introduced in IDX2, for the sliding surface introduced in IDX1.

YSURF

Y coordinate of the point introduced in IDX2, for the sliding surface introduced in IDX1.

 

Lab1= RES

~CFGET, Par, SLOPE, , RES, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to results. The data available for retrieve will be introduced in parameter Lab2.

Lab2

Description

F

Safety factor obtained, for the sliding surface introduced in IDX2 and for the movement indicated in IDX1 (IDX1=1 slides towards the left side IDX1=2 slides towards the right side).

WORST

Indicates the number of the sliding surface with the lowest safety factor for the movement indicated in IDX1 (IDX1=1 slides towards the left side IDX1=2 slides towards the right side).

 

Lab1= RE

~CFGET, Par, SLOPE, , RE, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the earth reinforcement group indicated in IDX1.

Lab2

Description

N

Number of bars and layers.

MU

Apparent friction coefficient.

FMAX

Strength of the bar (force).

F

Maximum force obtained.

FIXED

= 0 The reinforcement is not fixed.

= 1 The reinforcement is fixed to the slope surface.

POINTS

Coordinates of the points that define the geometry of the group.

IDX2 is the number of the point as shown in the diagram.

Lab3 = X or Y to retrieve the X or Y coordinate.

 

·         ~CFGET – FOUNDAT (ENTNUM is the foundation number)

 

~CFGET, Par, FOUNDAT, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= ELEMLab3, IDX1, IDX2, IDX3

Retrieves general data relative to the elements of the foundation introduced in field ENTNUM. The data available for retrieve will be introduced in parameter Lab2.

Lab2

Description

COUNT

Number of foundation elements.

EFS

Ballast module of the element introduced in IDX1.

NODE

Node number according to ANSYS to which it corresponds the local node number (nnode) introduced in IDX2 of the element introduced in IDX1.

1 £ nnode £ 8

 

Lab1= NODE

~CFGET, Par, FOUNDAT, ENTNUM, NODE, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the nodes of the elements of the foundation introduced in field ENTNUM. The data available for retrieve will be introduced in parameter Lab2.

Lab2

Description

COUNT

Number of foundation nodes.

EFS

Ballast module of the node introduced in IDX1.

X

X coordinate of the node introduced in IDX1.

Y

Y coordinate of the node introduced in IDX1.

Z

Z coordinate of the node introduced in IDX1.

MAX

Node with maximum ballast module.

MIN

Node with minimum ballast module.

MED

Node with ballast module closest to the mean value.

 

Lab1= MAT

~CFGET, Par, FOUNDAT, ENTNUM, MAT, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the soil materials that have an influence on the foundation introduced in field ENTNUM. The data available for retrieve will be introduced in parameter Lab2.

Lab2

Description

EM

Mean elastic modulus.

NUM

Mean Poisson coefficient.

 

Lab1= EFS

~CFGET, Par, FOUNDAT, ENTNUM, EFS, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the elastic foundation stiffness corresponding to the foundation introduced in field ENTNUM. The data available to retrieve will be introduced in parameter Lab2.

Lab2

Description

MAX

Maximum ballast module in the foundation.

MIN

Minimum ballast module in the foundation.

MED

Mean ballast module in the foundation.

 

 

·         ~CFGET – TERRAIN (ENTNUM is the foundation number)

 

~CFGET, Par, TERRAIN, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= LAYER

~CFGET, Par, TERRAIN, ENTNUM, LAYER, Lab2, , IDX1, IDX2, IDX3

Recovers data relative to terrain layers specified in ENTNUM. The different data to recover is introduced in the Lab2 label.

Lab2

Description

COUNT

Number of layers that form the terrain.

MAT

Number of the associated material to the layer introduced in IDX1.

THK

Thickness of layer introduced in IDX1.

HBM

 Horizontal Ballast module of the layer introduced in IDX1.

KSEL

Type of earth pressure in the layer introduced in IDX1:

KSEL=DB

Ranking Theory to calculate the earth pressure

KSEL=CLMB

Coulomb Theory to calculate the earth pressure

 

Lab1= KCN

~CFGET, Par, TERRAIN, ENTNUM, KCN, , , IDX1, IDX2, IDX3

Reference number of the axis system where the terrain is being defined.

 

Lab1= DIR

~CFGET, Par, TERRAIN, ENTNUM, DIR, , , IDX1, IDX2, IDX3

Direction of the height axis of the terrain.

 

Lab1= SURFLV

~CFGET, Par, TERRAIN, ENTNUM, SURFLV, , , IDX1, IDX2, IDX3

 Upper terrain height.

 

Lab1= WKEY

~CFGET, Par, TERRAIN, ENTNUM, WKEY, , , IDX1, IDX2, IDX3

Identifies ground-water level influence (0 – Does not consider the ground-water level, 1 – Takes into account the ground-water level).

 

Lab1= WH

~CFGET, Par, TERRAIN, ENTNUM, WH, , , IDX1, IDX2, IDX3

Height of the ground-water level.

 

Lab1= BETA

~CFGET, Par, TERRAIN, ENTNUM, BETA, , , IDX1, IDX2, IDX3

Angle of the terrain slope (sexagesimal degrees).

 

Lab1= Q

~CFGET, Par, TERRAIN, ENTNUM, Q, , , IDX1, IDX2, IDX3

Surface load.

 

Lab1= NAME

~CFGET, Par, TERRAIN, ENTNUM, NAME, , , IDX1, IDX2, IDX3

Name of the terrain. IDX1 indicates the eight-character group to recover. If the name is longer than eight characters, the following eight will be recovered indicating in IDX1 the next group. Due that the maximum number of characters is 32 IDX1 can take as values 1, 2, 3 or 4.

 

·         ~CFGET – WALL (ENTNUM is not used)

~CFGET, Par, WALL, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= UTER

~CFGET, Par, WALL, , UTER, , , IDX1, IDX2, IDX3

Retrieves the associated terrain to the retaining wall. The retaining wall number is specified in IDX1.

 

Lab1= NSEC

~CFGET, Par, WALL, , NSEC, , , IDX1, IDX2, IDX3

Number of sections that define the retaining wall. The retaining wall number is specified in IDX1.

 

Lab1= NSTEP

~CFGET, Par, WALL, , NSTEP, , , IDX1, IDX2, IDX3

Number of calculus steps.

 

Lab1= NWALL

~CFGET, Par, WALL, , NWALL, , , IDX1, IDX2, IDX3

Number of retaining walls.

 

Lab1= COORD

~CFGET, Par, WALL, , COORD, Lab2, , , IDX1, IDX2, IDX3

Recovers data relative to the retaining wall coordinates. The different data to recover is introduced in the Lab2 label.

Lab2

Description

X

X coordinate of the retaining wall.

YMAX

Y max coordinate of the retaining wall

YMIN

Y min coordinate of the retaining wall

 

·         ~CFGET – BRIDGE (ENTNUM is not used)

~CFGET, Par, BRIDGE, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= VEHICLE

~CFGET, Par, BRIDGE, , VEHICLE, Lab2, , , IDX1, IDX2, IDX3

Recovers data relative to the bridge module. The different data to retrieve is introduced in the Lab2 label

Lab2

Description

ROWS

Wheels rows number. The number of the vehicle is specified in IDX1.

COLS

Wheels columns number. The number of the vehicle is specified in IDX1

TYPE

Vehicle type. The vehicle number is specified in IDX1.

0

Rigid

1

Flexible

D

Exempt distance after the vehicle has pass. The number of the vehicle is specified in IDX1

START

Part of the vehicle that remains out of the bridge at beginning of the generation. The vehicle number is specified in IDX1

END

Part of the vehicle that remains over the bridge at beginning of the generation. The vehicle number is specified in IDX1

LOC

 Coordinates of the centre. The coordinates to obtain (X,Y) are indicated in Lab 3. The vehicle number is specified in IDX1

CSP

Spacing between columns. The vehicle number is specified in IDX1.The column number is introduced in IDX2.

RSP

 Spacing between rows. The vehicle number is specified in I IDX1. The row number is introduced in IDX2.

Q

Loads per wheel. The vehicle number is specified in IDX1. The row number is introduced in IDX2.The column number is introduced in IDX3.

NUMBER

Number of vehicles.

MAX

Higher number of vehicle defined

NAME

Name of the vehicle. The vehicle number is specified in IDX1.

 

Lab1= FAMILY

~CFGET, Par, BRIDGE, , FAMILY, Lab2, , , IDX1, IDX2, IDX3

 Recovers data relative to the defined families. The different data to recover is introduced in the Lab2 label.

Lab2

Description

TYPE

Type of family. The family number is specified in IDX1.

1

Addition.

2

Addition with variable coefficients.

3

Incompatible or exclusive.

4

Compatible.

5

Option.

6

Opposite.

7

Selection.

8

Selection with variable coefficients.

NLDCOMB

Maximum number of loads that can take part of an internal combination. The number of the family is specified in IDX1.

NSTATES

Number of start states that compose the family. The number of the family is specified in IDX1.

COEFT1I

Multiplier Coefficient to apply to the load in the internal combinations when the load is favourable. The number of the family is specified in IDX1.

COEFT2I

Multiplier Coefficient to apply to the load in the internal combinations when the load is unfavourable. The number of the family is specified in IDX1..

STATES

Start States that compose the family. The number of the family is specified in IDX1.

NUMBER

Number of families.

MAX

Highest number of Family defined

 

Lab1= CABLE

~CFGET, Par, BRIDGE, , CABLE, Lab2, Lab3, IDX1, IDX2, IDX3

 Retrieves data relative to the defined prestressed cables. The different data to recover is introduced in the Lab2 label.

Lab2

Description

NPTS

Number of points. The cable number is specified in IDX1.

LS

Load step in which has been introduced. If it is zero, indicates that load step is not yet defined. The cable number is specified in IDX1 and the point number in IDX2

LOC

Coordinates of the point. The coordinates to obtain (X,Y,Z) are indicated in Lab 3. The cable number is specified in IDX1 and the point number in IDX2.

TGIN

Vector tangent to the stretch following the point. The coordinates to obtain (X,Y,Z) are indicated in Lab 3. The cable number is specified in IDX1 and the point number in IDX2.

TGOUT

Vector tangent to the stretch following the point. The coordinates to obtain (X,Y,Z) are indicated in Lab 3. The cable number is specified in IDX1 and the point number in IDX2.

TENSION

Cable tension in each point. The cable number is specified in IDX1 and the point number in IDX2.

NUMBER

Number of cables.

MAX

Highest number of cable defined

 

Lab1= SECTION

~CFGET, Par, BRIDGE, , SECTION, Lab2, Lab3, IDX1, IDX2, IDX3

Retrieves data relative to the defined bridge cross sections. The different data to recover is introduced in the Lab2 label.

Lab2

Description

TYPE

Section type. The section number is specified in IDX1. Available only for slab section.

Section type

Returned value

RS

1

TS

2

TF

3

PS

4

PAL

5

PAR

6

MAT

Section’s material. The section number is specified in IDX1.

NAME

Name of the section. The section number is specified in IDX1.

NPOINT

Number of points in the cross section. The section number is specified in IDX1. Available only for slab sections.

NHOLES

Number of holes in the cross section. The section number is specified in IDX1. Available only for slab sections.

NDIV

Number of divisions in the cross section. The section number is specified in IDX1. Available only for slab sections.

POINT

Point coordinates. Available only for slab sections.

Lab3

Description

Y

Y coordinate of the point

Z

Z coordinate of the point

The section number is specified in IDX1 and the point in IDX2.

HOLES

Coordinates of the hole’s center. Available only for slab sections.

Lab3

Description

YCENT

Y coordinate of the point

ZCENT

Z coordinate of the point

The section number is specified in IDX1 and the hole number in IDX2.

DIV

Number of division point. Available only for slab sections.

Lab3

Description

TOP

Top division point

BOT

Bottom division point

SUPPORT

Dvision point at support

The cross section is specified in IDX1 and the division number in IDX2.

DIM

Value of the dimension of slab section IDX1. The dimension index is specified in IDX2 as it is described in the ~BRSSLAB parameters

SHP

Section shape. The section number is specified in IDX1.

1

Slab

2

Box

NCELL

Number of cells in section IDX1. Available only for box sections.

KSYM

Section IDX1 symmetry condition. Available only for box sections.

0

Non symmetric section

1

Symmetric section, the command takes into account to left side of the section

-1

Symmetric section, the command takes into account to right side of the section

CELL

Cell data. Available only for box sections.

Lab3

Description

WIDTH

Cell width

THTOP

Top thickness

THBOT

Bottom thickness

The section number is specified in IDX1 and the cell number in IDX2.

WEB

Web data. Available only for box sections.

Lab3

Description

DEPTH

Web depth

THICK

Web thicness

SLOPE

Web slope relative to vertical plane

RATS

Web ratio

SLPS

Web slope

RATB

Bracket ratio

SLPB

Bracket slope

The section number is specified in IDX1 and the web number in IDX2.

IDX3

Location in the web

1

Left top

2

Right top

3

Left bottom

4

Right bottom

FLANGE

Flange section data. Available only for box sections.

Lab3

Description

LENGTH

Flange length

THICK

Flange thickness

The section number is specified in IDX1 and the flange number in IDX2.

IDX2

Flange

1

Left top

2

Right top

3

Left bottom

4

Right bottom

CROWN

Crown data. Available only for box sections.

Lab3

Description

THINCR

Crown over-thickness

RATIO

Crown vertex position relative to bridge width.

 

Lab1= SMODEL

~CFGET, Par, BRIDGE, , SMODEL, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the bridge solid modelling. The different data to recover is introduced in the Lab2 label.

Lab2

Description

COUNT

Gives the number of cross sections used in the solid modelling.

MP

Value of MP associated to the cross section. The MP number of the solid modelling is introduced in IDX1.

NSEC

Section number. The cross section number used in the solid modelling is introduced in IDX1. If the value is 0, the program calculates it.

YOFF

Offset in Y. The point of the solid modelling at which the value of the Y offset is to be retrieved is introduced in IDX1.

ZOFF

Offset in Z. The point of the solid modelling at which the value of the Z offset is to be retrieved is introduced in IDX1.

BANK

Bank. The point of the solid modelling at which the value of the bank is to be retrieved is introduced in IDX1

SKEW

Skew angle. The point of the solid modelling at which the value of the skew angle is to be retrieved is introduced in IDX1.

TRANS

Transition between cross sections of the solid model. The point of the solid modelling at which the type of transition used is to be retrieved, is introduced in IDX1.

CSYS

Local coordinate system associated to ANSYS. The point of the solid modelling at which the local coordinate system is to be retrieved is introduced in IDX1.

SOLID

Identifies if the cross section used in the model is solid or hollow. The point of the solid modelling, at which the type of cross section used is to be retrieved, is introduced in IDX1. The output will be 0 for hollow sections and ¹0 if solid.

 

Lab1= STRETCH

~CFGET, Par, BRIDGE, , STRETCH, Lab2, Lab3, IDX1, IDX2, IDX3

Retrieves data relative to the bridge stretch. The different data to recover is introduced in the Lab2 label.

Lab2

Description

PLANT

Stretch in plan view.

Lab3

Description

COUNT

Number of stretches in plan view.

MP

Mileage point. The stretch number is introduced IDX1 and the end value (1 for end i and 2 for end j) is introduced in IDX2.

TYPE

Type of stretch. The stretch number is introduced in IDX1 and the program will output the following values: 1 – straight line, 2 - arch, 3 - clothoid

PARAM

Parameters. The stretch number is introduced in IDX1. In the event of an arch line, the program gives the user the value of the radius. If it is a clothoid, the program gives the user the value of the parameter (A) of the clothoid, always positive in the counterclockwise direction.

ANG

Angle with respect to the previous stretch. The stretch number is introduced in IDX1.

RAD

Radius of curvature at ends. The stretch number is introduced in IDX1 and the end value (1 for end i and 2 for end j) is introduced in IDX2.

ELEV

Point number at the cross section division.

Lab3

Description

COUNT

Number of stretches in elevation.

MP

Mileage point. The stretch number is introduced IDX1 and the end value (1 for end i and 2 for end j) is introduced in IDX2.

M

Slope at each end, given in %. The stretch number is introduced in IDX1 and the end value (1 for end i and 2 for end j) is introduced in IDX2.

TYPE

Type of stretch. The stretch number is introduced in IDX1 and the program will output the following values: 1 - straight line, 2 – parabola.

KV

Parameter of the parabola. The stretch number is introduced in IDX1.

PINI

XYZ Coordinates XYZ of initial point. The chosen coordinate is introduced in IDX1. If the value is 1, the program will output the X coordinate of the initial point, if 2 the Y coordinate and 3 for Z coordinate.

VINI

XYZ Coordinates of the initial tangent vector. The chosen coordinate is introduced in IDX1. If the value is 1, the program will output the X coordinate of the initial tangent vector, if 2 the Y coordinate and 3 for Z coordinate.

 

 

·         ~CFGET – PRSCONC (ENTNUM is not used)

~CFGET, Par, PRSCONC, ENTNUM, Lab1, Lab2, Lab3, IDX1, IDX2, IDX3

 

Lab1= SBEAM

~CFGET, Par, PRSCONC, , SBEAM, Lab2, , IDX1, IDX2, IDX3

Retrieves data relative to the support beam. The different data to retrieve is introduced in the Lab2 label.

Lab2

Description

TYPE

Prestressing type (pre or post-tensioned).

CSYS

Active coordinate system where the support beam is captured.

NTN

Number of defined tendons.

NCUT

Number of support beam cuts.

NPTY

Number of control points of the elevation view.

NPTZ

Number of control points of the plan view.

 

Lab1= TENDON

~CFGET, Par, PRSCONC, , TENDON, Lab2, Lab3, IDX1, IDX2, IDX3

Retrieves data relative to the defined tendons. The different data to retrieve is introduced in the Lab2 label.

Lab2

Lab3

Description

COUNT

 

Number of defined tendons.

MAT

 

Material number of tendon IDX1.

ACTIVE

 

Condition of tendon IDX1.

1

Active

0

Inactive

PNPTS

 

Number of points in plan view of tendon IDX1.

ENPTS

 

Number of points in elevation view of tendon IDX1.

ORDER

 

Prestressing order of tendon IDX1.

AREA

 

Area of tendon IDX1.

DIAMETER

 

Diameter of the tendon IDX1 casing.

P0MAX

 

Initial force of tendon IDX1.

P0

 

Anchorage force of tendon IDX1.

METHOD

 

Prestressing sequence of tendon IDX1:

0

Both ends are prestressed at the same time

1

On the left end

2

On the right end

3

First on the left and after on the right end

4

First on the right and after on the left end

PPOINTS

 

User-defined number for the point in plan view of tendon IDX1 located at the position IDX2.

EPOINTS

 

User-defined number for the point in elevation view of tendon IDX1 located at the position IDX2.

LOSS

 

Losses of prestressing of tendon IDX1 at cut IDX2.The type of prestressing losses is specified at IDX3 and depends on the prestressing type:

Pre-tensioned:

1

Steel relaxation losses before transfer and due to heating.

2

Thermal expansion losses.

3

Slippage in the anchorage.

4

Elastic shortening of concrete.

5

Concrete shrinkage losses.

6

Concrete creep losses

7

Losses due steel relaxation

Post-tensioned:

1

Friction losses.

2

Slippage in the anchorage.

3

Elastic shortening of concrete.

4

Concrete shrinkage losses.

5

Concrete creep losses

6

Losses due steel relaxation

COORD

 

IDX1: Tendon number.
IDX2: Cut number.

 

X

X coordinate of the tendon in this cut.

 

Y

Y coordinate of the tendon in this cut.

 

Z

Z coordinate of the tendon in this cut.

 

SXY

Tendon’s slope of XY plane.

 

SXZ

Tendon’s slope of XZ plane.

 

Lab1= CUT

~CFGET, Par, PRSCONC, , CUT, Lab2, , IDX1, IDX2, IDX3

Retrieves the data related to the cuts of the support beam. The different data to retrieve is introduced in the Lab2 label.

Lab2

Description

COUNT

Number of cuts.

X

X coordinate of the cut IDX1 in the section coordinate system.

Y

Y coordinate of the cut IDX1 in the section coordinate system

Z

Z coordinate of the cut IDX1 in the section coordinate system

DIST

Distance from the beginning of the support beam to the cut IDX1.

UPCOVER

Top cover of cut IDX1.

BOTCOVER

Bottom cover of cut IDX1

NODE

Node associated to cut IDX1 (only for beam models).

LOSS

Prestressing losses of tendon IDX1 at cut IDX2. The types of prestressing losses are specified at IDX3 and depends on the prestressing type:

Pre-tensioned:

1

Steel relaxation losses before transfer and due to heating.

2

Thermal expansion losses.

3

Slippage in the anchorage.

4

Elastic shortening of concrete.

5

Concrete shrinkage losses.

6

Concrete creep losses

7

Losses due steel relaxation

Post-tensioned:

1

Friction losses.

2

Slippage in the anchorage.

3

Elastic shortening of concrete.

4

Concrete shrinkage losses.

5

Concrete creep losses

6

Losses due steel relaxation

 

Lab1= NODE

~CFGET, Par, PRSCONC, , NODE, Lab2, , IDX1, IDX2, IDX3

Retrieves the data related to the nodes associated to the support beam. The different data to retrieve is introduced in the Lab2 label.

Lab2

Description

CUT

Cut associated to the node IDX1 (only for beam models)

 

Lab1= PPOINT

~CFGET, Par, PRSCONC, , PPOINT, Lab2, , IDX1, IDX2, IDX3

Retrieves the data related to the tendon’s points in plan view. The different data to retrieve is introduced in the Lab2 label.

Lab2

Description

COUNT

Number of points in plan view.

X

X coordinate of point IDX1 with respect to the origin of the support beam.

Y

Y coordinate of point IDX1 with respect to the section coordinate system.

Z

Y coordinate of point IDX1 with respect to the section coordinate system.

SLOPE

Slope defined in point IDX1.

INFDIST

Distance ratio of the inflection point of the tendon segment following point IDX1 (see ~PCPPDEF command).

CUT

Cut over which the point IDX1 is located.

 

Lab1= EPOINT

~CFGET, Par, PRSCONC, , EPOINT, Lab2, , IDX1, IDX2, IDX3

Retrieves the data related to the tendon’s points in elevation view. The different data to retrieve is introduced in the Lab2 label.

Lab2

Description

COUNT

Number of points in elevation view.

X

X coordinate of point IDX1 with respect to the origin of the support beam.

Y

Y coordinate of point IDX1 with respect to the section coordinate system.

Z

Y coordinate of point IDX1 with respect to the section coordinate system.

SLOPE

Slope defined in point IDX1.

INFDIST

Distance ratio of the inflection point of the tendon segment following point IDX1 (see ~PCEPDEF command).

CUT

Cut over which the point IDX1 is located.

 

Lab1= STLOSS

~CFGET, Par, PRSCONC, , STLOSS, Lab2, , IDX1, IDX2, IDX3

Retrieves the data related to the immediate prestressing losses calculation. The different data to retrieve is introduced in the Lab2 label.

Lab2

Description

RELAX

Calculation type of initial steel relaxation losses:

USER

Set by user.

NONE

Not considerable.

AUTO

Calculated by the CivilFEM.

K

Thermal reduction factor.

LVAL

Heating temperature variation.

 

Lab1= LTLOSS

~CFGET, Par, PRSCONC, , LTLOSS, Lab2, , IDX1, IDX2, IDX3

Retrieves the data related to the long term prestressing losses calculation. The different data to retrieve is introduced in the Lab2 label.

Lab2

Description

LTAGE

Calculation time for the long-term losses.

KOPT

Losses calculation type:

0

Independent

1

Aproximated coupling

LABOPT

Formulation used.

LVAL

Value that depends on the calculation options (see ~PCLOSS command).

 

 

·         ~CFGET – FRAME

~CFGET, Par, FRAME, ENTNUM, Lab1, , , IDX1, IDX2, IDX3

 

Lab1= NAME

~CFGET, Par, FRAME, ENTNUM, NAME , , , IDX1

Name assigned to the frame (32 characters). IDX1 indicates the group of 8 characters to recover.

IDX1

Characters

1

1 to 8

2

9 to 16

3

17 to 24

4

25 to 32

 

Lab1= H

~CFGET, Par, FRAME, ENTNUM, H

Free height between slab and lintel.

 

Lab1= L

~CFGET, Par, FRAME, ENTNUM, L

Distance between piers.

 

Lab1= PTH

~CFGET, Par, FRAME, ENTNUM, PTH

Pier thickness.

 

Lab1= LTH

~CFGET, Par, FRAME, ENTNUM, LTH

Lintel thickness.

 

Lab1= STH

~CFGET, Par, FRAME, ENTNUM, STH

Slab thickness.

 

Lab1= LF

~CFGET, Par, FRAME, ENTNUM, LF

Left flange length.

 

Lab1= RF

~CFGET, Par, FRAME, ENTNUM, RF

Rigth flange length.

 

Lab1= HU

~CFGET, Par, FRAME, ENTNUM, HU

Vertical projection of the upper brackets

 

Lab1= VU

~CFGET, Par, FRAME, ENTNUM, VU

Horizontal projection of the upper brackets.

 

Lab1= HD

~CFGET, Par, FRAME, ENTNUM, HD

Vertical projection of the lower brackets

 

Lab1= VD

~CFGET, Par, FRAME, ENTNUM, VD

Horizontal projection of the lower brackets.

 

Lab1= HL

~CFGET, Par, FRAME, ENTNUM, HL

Terrain height over the lintel.

 

Lab1= HS

~CFGET, Par, FRAME, ENTNUM, HS

Terrain height over the slab.

 

Lab1= TGAMMA

~CFGET, Par, FRAME, ENTNUM, TGAMMA

Terrain specific weight.

 

Lab1= ST

~CFGET, Par, FRAME, ENTNUM, ST

Terrain mean stress in frames.

 

Lab1= FRIC

~CFGET, Par, FRAME, ENTNUM, FRIC

Terrain internal friction angle.

 

Lab1= KFS

~CFGET, Par, FRAME, ENTNUM, KFS

Balast module.

 

Lab1= REC

~CFGET, Par, FRAME, ENTNUM, REC

Geometrical cover.

 

Lab1= SEP

~CFGET, Par, FRAME, ENTNUM, SEP, , , IDX1, IDX2

Distance between reinforcements.

 

Lab1= FI

~CFGET, Par, FRAME, ENTNUM, FI, , , IDX1, IDX2

Diameter of the reinforcements.

 

Lab1= BENT

~CFGET, Par, FRAME, ENTNUM, BENT,,, IDX1, IDX2

Bending length.

 

Lab1= FOUND

~CFGET, Par, FRAME, ENTNUM, FOUND,,, IDX1

Length of the concrete foundations.

 

 

·         ~CFGET – SEISM (ENTNUM = 0 or blank)

 

~CFGET, Par, SEISM, 0, Lab1, Lab2,, IDX1, IDX2,

 

Lab1 = NMODES

~CFGET, Par, SEISM, 0, NMODES

Number of modes extracted.

 

Lab1 = COMP

~CFGET, Par, SEISM, 0, COMP,,, IDX1

Spectrum component applied to each direction.

IDX1

Description

1

X direction

2

Y direction

3

Z direction

 

 

Lab1 = XDIR

~CFGET, Par, SEISM, 0, XDIR,,, IDX1

Components of the X-direction vector.

IDX1

Description

1

X component

2

Y component

3

Z component

 

 

Lab1 = YDIR

~CFGET, Par, SEISM, 0, YDIR,,, IDX1

Components of the Y-direction vector.

IDX1

Description

1

X component

2

Y component

3

Z component

 

 

Lab1 = ZDIR

~CFGET, Par, SEISM, 0, ZDIR,,, IDX1

Components of the Z-direction vector.

IDX1

Description

1

X component

2

Y component

3

Z component

 

 

Lab1 = COMP

~CFGET, Par, SEISM, 0, TYPE,,, IDX1

Spectrum type selected. Must be 1 or 2 according to the code used.

 

Lab1 = SPECT

~CFGET, Par, SEISM, 0, SPECT, Lab2,, IDX1, IDX2, IDX3

Data of the spectrum number IDX1.

 

Lab2

Description

NPTH

Number of defined points for the horizontal spectrum.

NPTV

Number of defined points for the vertical spectrum.

DAMP

Damping for which the spectrum has been defined.

TH

Periods for horizontal spectrum. IDX2 = 1, NPTH

IDX3

Description

1

1st spectrum (code dependant)

2

2nd spectrum (code dependant)

SDH

Values of the horizontal spectrum. IDX2 = 1, NPTH

IDX3

Description

1

1st spectrum (code dependant)

2

2nd spectrum (code dependant)

TV

Periods for vertical spectrum. IDX2 = 1, NPTV

IDX3

Description

1

1st spectrum (code dependant)

2

2nd spectrum (code dependant)

SDV

Values of the vertical spectrum. IDX2 = 1, NPTV

IDX3

Description

1

1st spectrum (code dependant)

2

2nd spectrum (code dependant)

 

Lab1 = MODE

~CFGET, Par, SEISM, 0, MODE, Lab2,,IDX1, IDX2

Data about the modal spectral analysis.

 

Lab2

Description

FREC

Frequency of mode IDX1

PERI

Period of mode IDX1

FACT

Participation factor of mode IDX1 for direction IDX2

IDX2

Direction

1

X

2

Y

3

Z

EFFM

Effective mass of mode IDX1 for direction IDX2

IDX2

Direction

1

X

2

Y

3

Z

 

Lab1 = PUSH

~CFGET, Par, SEISM, 0, PUSH, Lab2,,IDX1, IDX2

Data about the Push Over analysis.

 

Lab2

Description

PP

Performance point

IDX2

Description

1

Sd

2

Sa

IP

Inelastic point

IDX2

Description

1

Sd

2

Sa

EP

Elastic point

IDX2

Description

1

Sd

2

Sa

NPTCSC

Number of points of the Capacity Spectrum Curve

NPTDSC

Number of points of the Demand Spectrum Curve

CSC

Capacity Spectrum Cuve. IDX1 = 1, NPTCSC

IDX2

Description

1

Sd

2

Sa

DSC

Demand Spectrum Cuve. IDX1 = 1, NPTDSC

IDX2

Description

1

Sd

2

Sa

 

Menu Path

This command is not available through menu.

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