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Chapter 6
CivilFEM Combinations

 

6.1                       CivilFEM Combinations

Through the CivilFEM the combinations module, the user can select a set of load cases and combine them in such a way to achieve targeted results. Therefore, the results combination is based on the search for a specific combination among a certain data set which adheres to a particular set of rules which will solve for the targets at every node of the system.

 

The combinations module can be used to solve problems such as the following example:

combi

Figure 6.1-1

As the figure illustrates, a beam with two supports is divided into elements and submitted to the actions of:

·         A vertical force F that can be placed at any node (but only one at any moment)

·         A uniform distributed load P that can act on any of the indicated elements (All, several, one, or none of them).

The objective is to search for the load distribution that will produce the most unfavorable load case using every node and element of the system. This load case will be used to calculate a target criterion, for example the maximum bending moment MZ. In this example, the worst load case will be found by determining where the force F (at which node) and the distributed load (on which element or elements) should be placed in order to obtain the maximum bending moment MZ. Once this value is calculated, the remaining forces and moments (FX, FY, FZ, MX and MY) that are obtained on the same node and with the same loads configuration are the designated as concomitant values.

Moreover, the vertical force F and the uniform distributed load P can be modified by variable factors that will increase or decrease their effect to achieve the most unfavorable case, as is common in code checks.

Other problem types that can be solved by the combinations module may be found in the Examples Manual.

Apart from using CivilFEM combination capabilities to obtain a desired target value, it is possible to obtain the results from every load case generated from the defined combination rules (command ~LINCMB). This chapter focuses on utilizing the module to find a target value. Chapter 6.10 explains the differences between searching for a target and obtaining all the possible load case results.

 

6.2                       Results Combination in ANSYS and in CivilFEM

The result combinations with ANSYS allow the user to utilize different result sets in an explicit way (Load Case). The user must define which result sets should be used and how they should be combined to obtain the desired result. The load case used to obtain the result will be the same for the whole model. Therefore, an example of an ANSYS load case would be the following:

            “LoadCase1 = 1.20 * LoadStep1 + 0.95 * LoadStep3”

However, in CivilFEM, a combination rule can be defined in an implicit way.  To be precise, the user can indicate which result sets or start states and what rules will be utilized in the combination. This combination will differ from the example above in that it will obtain certain targets or criteria for each node of the model. Therefore, it is possible to define a combination rule as:

Combination1 = Add two load cases chosen between [ (1.20 or 0.95) * LoadStep1,  (0.95 or 0.00) * LoadStep2,  (0.95 or 0.75) * LoadStep3 ]

Logically, the previously definition for combination1 allows 12 possibilities:

            Combination1 = 1.20 * LoadStep1 + 0.95 * LoadStep2

            Combination1 = 1.20 * LoadStep1 + 0.95 * LoadStep3

            Combination1 = 0.95 * LoadStep2 + 0.95 * LoadStep3

            Combination1 = 0.95 * LoadStep1 + 0.95 * LoadStep2

            Combination1 = 0.95 * LoadStep1 + 0.95 * LoadStep3

            Combination1 = 0.00 * LoadStep2 + 0.95 * LoadStep3

            Combination1 = 0.95 * LoadStep2 + 0.75 * LoadStep3

            ...

            Combination1 = 0.00 * LoadStep2 + 0.75 * LoadStep3

In addition, it will be necessary to specify the desired target or criterion for the combinations to calculate. This target will be determined by selecting extreme values from all of the possible load combinations (moments and forces, stresses, etc.). 

At each point, the selection procedure is independent of the selections at other points of the structure, and each procedure combines the results in a different way to achieve the target. For example, if one of the requested extreme values is maximum SX, this value could be obtained at vertex J of a certain element as:

            SXCombination1 = 1.20 * SXLoadStep1 + 0.95 *SX LoadStep2

and at vertex K of the same element as:

            SXCombination1 = 0.95 * SXLoadStep1 + 0.00 *SX LoadStep2

With ANSYS’ combination calculations, the SX value at a certain point of the structure will only have one value. However, in CivilFEM, different targets may be defined for the same combination rule; therefore, SX will have as many values as the number of extreme values or targets desired for that point. In addition to the target value, CivilFEM provides the concomitant results for each point of the structure.

When combinations are performed with ANSYS, each one of the Load Cases or combinations defined is written in an independent file jobname.LCxx. However, the combination rules created by the CivilFEM combinations module will be written in a unique results file called jobname.CMB or jobname.CVMB, depending on if the results come from the ANSYS results file (jobname.RST) or from the CivilFEM results file (jobname.RCV).

To read the results of a certain Data Set from RST file, the SET command is used, and to read the results of a Load Case calculated by ANSYS, the LCASE command is used. To read results of a combination rule created by CivilFEM, use the ~CMB or ~CFSET command after pointing to the combined results (see ~CMBDAT command).

6.3                       Basic Terminology

To begin, CivilFEM combinations module requires two initial data sets defined by the user:

1.    Targets are extreme values or desired values from the results that must be calculated at each point of the structure, for example:

 TARGET1 = Maximum Z bending moment (MZ+)”

 TARGET2 = Minimum X stress (SX-)”

 TARGET5 = Maximum Y shear in absolute value. (FY*)”

 ...

2.    The combination rules are the conditions that control how the program combines the different Load Cases in order to achieve the extreme values or Targets. For example:

“Combination1 = Add two load cases chosen between [ (1.20 or 0.95) *  LoadStep1,  (0.95 or 0.00) *  LoadStep2,  (0.95 or 0.75) * LoadStep3]”

“Combination2 = (1.00 or -1.00) * Combination1”

 ...

In the combination process, the program will follow the rules specified to produce target values at each point independently from the other points of the structure.  Therefore, a result set will be achieved by combining the start states in a different way for each point.

All the basic results provided by ANSYS or the CivilFEM postprocessor are categorized into different data groups for their use in the combinations module. Within a chosen data group, targets and concomitance values will be calculated.  These concomitance values will be the data in the group remaining values that does not pertain to the selected targets. For example, the BEAM data group includes forces, moments, stresses and strains in beam elements, that is: FX, FY, FZ, MX, MY, MZ, SDIR, SBYT, SBYB, SBZT, SBZB, EPELDIR, EPELBYT, EPELBYB, EPELBZT, EPELBZB. Therefore, if one of the Targets or desired result values is the maximum MZ (MZ+) bending moment, the program will obtain the maximum MZ moment and, simultaneously, the concomitant values FX, FY, FZ, MX, MY, SDIR, SBYT, SBYB, SBZT, SBZB, EPELDIR, EPELBYT, EPELBYB, EPELBZT, EPELBZB, of the same group.

A complete description of all the groups and their data can be found in Chapter 6.5.

A target is defined by the datum it refers to (for example MX) and by its TYPE (Minimum, Maximum or Maximum in absolute value) using the ~TRGDEF command.

A combination rule is defined by its Start States and by the way in which the Start States are combined using the ~CMBDEF, ~STSTDEF and ~STSTCFT commands.

6.4                       Types of Combination Rules

The types of COMBINATION rules that can be defined are:

Addition [ADD]

Addition with Variable Coefficients [ADDVC]

Incompatible or Exclusive Start States [INCOMPAT]

Compatible Start States [COMPATIB]

Optional Start States [OPTION]

Opposed Start States [OPOSED]

Selection of Start States [SELECT]

Selection of Start States with variable coefficients [SELECTVC]

6.4.1                      Addition

Every Start State is added with fixed coefficients. Each Start State is only multiplied by one coefficient. This rule uses classic addition, equivalent to the combinations with ANSYS.

6.4.2                      Addition with Variable Coefficients

Start States are added with variable coefficients. A maximum and minimum combination coefficient is assigned to each Start State. This rule can be used for combinations according to codes, for example, C = gfg · G + gfq · Q.

6.4.3                      Incompatible or Exclusive Start States

Either a maximum Start State is selected from the defined states or no state is selected. It is not necessary to define coefficients. This rule is used as a representation of mobile loads that can only be placed in only one position at a given time.

6.4.4                      Compatible Start States

Any Start State subset can be added together (all, many, one, or none of them). Coefficients are not necessary. This rule is used to represent live loads that can occur simultaneously (surface loads).

6.4.5                      Optional Start States

Only one of the Start States is selected. Coefficients are not necessary. This rule is useful for selecting among different Start States. For example, different locations of a load on a pile, different code Start States, etc.

6.4.6                      Opposed Start States

All the Start States of the combination are added, but each are multiplied by a maximum coefficient equal to +1 or a minimum coefficient equal to –1. This rule is useful for loads that act distinctly in two opposite directions (wind, earthquakes, etc.).

6.4.7                      Selection of Start States

A fixed number of Start States, selected among the ones defined, is added. The number of Start States to be added is required input, not the coefficients. This rule is used for moveable loads that can act in more than one position.

6.4.8                      Selection of Start States with Variable Coefficients

A fixed number of Start States are added and each one of them can be multiplied by two coefficients. Input requirements are the two coefficients per Start State and the number of Start States to be added. This is the most general type, but with degeneration it adapts to any of the previous types as shown in the table below.

 

TYPE

Coefficient

Number of Start States to add

Maximum

Minimum

ADD

C1*

C2 = C1

ALL

ADDVC

C1*

C2*

ALL

INCOMPAT

0

1

1

COMPATIB

0

1

ALL

OPTION

1

1

1

OPOSED

1

-1

ALL

SELECT

1

1

NADD*

SELECTVC

C1*

C2*

NADD*

* This data should be introduced by the user by means of ~CMBDEF and ~STSTCFT commands.

 

6.5                       Data Groups

The determination of whether data a concomitant value or a target value is established at group level. A data group is the results set obtained by ANSYS or CivilFEM at a point of the model (node or vertex of an element for ANSYS or an element end for CivilFEM).

The elements implemented for each one of the groups are:

- Data relative to elements (obtained by ANSYS)

1.   Beam elements group:
Link1, Beam3, Beam4, Link8, Link10, Pipe16, Pipe20, Beam23, Beam24, Beam44, Beam54, Beam188, Beam189

2.   Shell elements group:
Shell43, Shell63 and Shell93

3.   Solid elements group:
Plane2, Plane25, Plane42, Solid45, Solid64, Solid65, Plane82, Plane83, Solid95, Plane145, Plane146

4.   Axial symmetric shells group:
Shell51, Shell61

- Data relative to nodes (obtained by ANSYS)

5.   Displacements Group

6.   Reactions Group

- Data relative to ends (obtained by CivilFEM)

7    Cross section Group

8    Shell vertices Group

The expected data groups and targets are the following:

6.5.1                      Targets Group for Beam Elements Type

Includes forces, moments, stresses, strains, stress combination, strain combination at beam elements.

Table 6.5-1 Beam Elements Type

Item

Component

Type

Label

F

X

MIN

FX-

F

Y

MIN

FY-

F

Z

MIN

FZ-

M

X

MIN

MX-

M

Y

MIN

MY-

M

Z

MIN

MZ-

S

DIR

MIN

SDIR-

S

BYT

MIN

SBYT-

S

BYB

MIN

SBYB-

S

BZT

MIN

SBZT-

S

BZB

MIN

SBZB-

EPEL

DIR

MIN

EPELDIR-

EPEL

BYT

MIN

EPELBYT-

EPEL

BYB

MIN

EPELBYB-

EPEL

BZT

MIN

EPELBZT-

EPEL

BZB

MIN

EPELBZB-

COMBS

YTZT

MIN

CMSYTZT-

COMBS

YTZM

MIN

CMSYTZM-

COMBS

YTZB

MIN

CMSYTZB-

COMBS

YMZT

MIN

CMSYMZT-

COMBS

YMZM

MIN

CMSYMZM-

COMBS

YMZB

MIN

CMSYMZB-

COMBS

YBZT

MIN

CMSYBZT-

COMBS

YBZM

MIN

CMSYBZM-

COMBS

YBZB

MIN

CMSYBZB-

COMBEPEL

YTZT

MIN

CMEYTZT-

COMBEPEL

YTZM

MIN

CMEYTZM-

COMBEPEL

YTZB

MIN

CMEYTZB-

COMBEPEL

YMZT

MIN

CMEYMZT-

COMBEPEL

YMZM

MIN

CMEYMZM-

COMBEPEL

YMZB

MIN

CMEYMZB-

COMBEPEL

YBZT

MIN

CMEYBZT-

COMBEPEL

YBZM

MIN

CMEYBZM-

COMBEPEL

YBZB

MIN

CMEYBZB-

F

X

MAX

FX+

F

Y

MAX

FY+

F

Z

MAX

FZ+

M

X

MAX

MX+

M

Y

MAX

MY+

M

Z

MAX

MZ+

S

DIR

MAX

SDIR+

S

BYT

MAX

SBYT+

S

BYB

MAX

SBYB+

S

BZT

MAX

SBZT+

S

BZB

MAX

SBZB+

EPEL

DIR

MAX

EPELDIR+

EPEL

BYT

MAX

EPELBYT+

EPEL

BYB

MAX

EPELBYB+

EPEL

BZT

MAX

EPELBZT+

EPEL

BZB

MAX

EPELBZB+

COMBS

YTZT

MAX

CMSYTZT+

COMBS

YTZM

MAX

CMSYTZM+

COMBS

YTZB

MAX

CMSYTZB+

COMBS

YMZT

MAX

CMSYMZT+

COMBS

YMZM

MAX

CMSYMZM+

COMBS

YMZB

MAX

CMSYMZB+

COMBS

YBZT

MAX

CMSYBZT+

COMBS

YBZM

MAX

CMSYBZM+

COMBS

YBZB

MAX

CMSYBZB+

COMBEPEL

YTZT

MAX

CMEYTZT+

COMBEPEL

YTZM

MAX

CMEYTZM+

COMBEPEL

YTZB

MAX

CMEYTZB+

COMBEPEL

YMZT

MAX

CMEYMZT+

COMBEPEL

YMZM

MAX

CMEYMZM+

COMBEPEL

YMZB

MAX

CMEYMZB+

COMBEPEL

YBZT

MAX

CMEYBZT+

COMBEPEL

YBZM

MAX

CMEYBZM+

COMBEPEL

YBZB

MAX

CMEYBZB+

F

X

ABS

FX*

F

Y

ABS

FY*

F

Z

ABS

FZ*

M

X

ABS

MX*

M

Y

ABS

MY*

M

Z

ABS

MZ*

S

DIR

ABS

SDIR*

S

BYT

ABS

SBYT*

S

BYB

ABS

SBYB*

S

BZT

ABS

SBZT*

S

BZB

ABS

SBZB*

EPEL

DIR

ABS

EPELDIR*

EPEL

BYT

ABS

EPELBYT*

EPEL

BYB

ABS

EPELBYB*

EPEL

BZT

ABS

EPELBZT*

EPEL

BZB

ABS

EPELBZB*

COMBS

YTZT

ABS

CMSYTZT*

COMBS

YTZM

ABS

CMSYTZM*

COMBS

YTZB

ABS

CMSYTZB*

COMBS

YMZT

ABS

CMSYMZT*

COMBS

YMZM

ABS

CMSYMZM*

COMBS

YMZB

ABS

CMSYMZB*

COMBS

YBZT

ABS

CMSYBZT*

COMBS

YBZM

ABS

CMSYBZM*

COMBS

YBZB

ABS

CMSYBZB*

COMBEPEL

YTZT

ABS

CMEYTZT*

COMBEPEL

YTZM

ABS

CMEYTZM*

COMBEPEL

YTZB

ABS

CMEYTZB*

COMBEPEL

YMZT

ABS

CMEYMZT*

COMBEPEL

YMZM

ABS

CMEYMZM*

COMBEPEL

YMZB

ABS

CMEYMZB*

COMBEPEL

YBZT

ABS

CMEYBZT*

COMBEPEL

YBZM

ABS

CMEYBZM*

COMBEPEL

YBZB

ABS

CMEYBZB*

 

6.5.2                      Targets Group for Shell Elements Type

Includes forces, moments, stresses and strains for a shell element type.

Table 6.5-2 Shell Elements Type

Item

Component

Type

Label

T

X

MIN

TX-

T

Y

MIN

TY-

T

XY

MIN

TXY-

M

X

MIN

MX-

M

Y

MIN

MY-

M

XY

MIN

MXY-

N

X

MIN

NX-

N

Y

MIN

NY-

S

XT

MIN

SXT-

S

YT

MIN

SYT-

S

ZT

MIN

SZT-

S

XYT

MIN

SXYT-

S

YZT

MIN

SYZT-

S

XZT

MIN

SXZT-

S

XB

MIN

SXB-

S

YB

MIN

SYB-

S

ZB

MIN

SZB-

S

XYB

MIN

SXYB-

S

YZB

MIN

SYZB-

S

XZB

MIN

SXZB-

EPEL

XT

MIN

EPELXT-

EPEL

YT

MIN

EPELYT-

EPEL

ZT

MIN

EPELZT-

EPEL

XYT

MIN

EPELXYT-

EPEL

YZT

MIN

EPELYZT-

EPEL

XZT

MIN

EPELXZT-

EPEL

XB

MIN

EPELXB-

EPEL

YB

MIN

EPELYB-

EPEL

ZB

MIN

EPELZB-

EPEL

XYB

MIN

EPELXYB-

EPEL

YZB

MIN

EPELYZB-

EPEL

XZB

MIN

EPELXZB-

T

X

MAX

TX+

T

Y

MAX

TY+

T

XY

MAX

TXY+

M

X

MAX

MX+

M

Y

MAX

MY+

M

XY

MAX

MXY+

N

X

MAX

NX+

N

Y

MAX

NY+

S

XT

MAX

SXT+

S

YT

MAX

SYT+

S

ZT

MAX

SZT+

S

XYT

MAX

SXYT+

S

YZT

MAX

SYZT+

S

XZT

MAX

SXZT+

S

XB

MAX

SXB+

S

YB

MAX

SYB+

S

ZB

MAX

SZB+

S

XYB

MAX

SXYB+

S

YZB

MAX

SYZB+

S

XZB

MAX

SXZB+

EPEL

XT

MAX

EPELXT+

EPEL

YT

MAX

EPELYT+

EPEL

ZT

MAX

EPELZT+

EPEL

XYT

MAX

EPELXYT+

EPEL

YZT

MAX

EPELYZT+

EPEL

XZT

MAX

EPELXZT+

EPEL

XB

MAX

EPELXB+

EPEL

YB

MAX

EPELYB+

EPEL

ZB

MAX

EPELZB+

EPEL

XYB

MAX

EPELXYB+

EPEL

YZB

MAX

EPELYZB+

EPEL

XZB

MAX

EPELXZB+

T

X

ABS

TX*

T

Y

ABS

TY*

T

XY

ABS

TXY*

M

X

ABS

MX*

M

Y

ABS

MY*

M

XY

ABS

MXY*

N

X

ABS

NX*

N

Y

ABS

NY*

S

XT

ABS

SXT*

S

YT

ABS

SYT*

S

ZT

ABS

SZT*

S

XYT

ABS

SXYT*

S

YZT

ABS

SYZT*

S

XZT

ABS

SXZT*

S

XB

ABS

SXB*

S

YB

ABS

SYB*

S

ZB

ABS

SZB*

S

XYB

ABS

SXYB*

S

YZB

ABS

SYZB*

S

XZB

ABS

SXZB*

EPEL

XT

ABS

EPELXT*

EPEL

YT

ABS

EPELYT*

EPEL

ZT

ABS

EPELZT*

EPEL

XYT

ABS

EPELXYT*

EPEL

YZT

ABS

EPELYZT*

EPEL

XZT

ABS

EPELXZT*

EPEL

XB

ABS

EPELXB*

EPEL

YB

ABS

EPELYB*

EPEL

ZB

ABS

EPELZB*

EPEL

XYB

ABS

EPELXYB*

EPEL

YZB

ABS

EPELYZB*

EPEL

XZB

ABS

EPELXZB*

 

6.5.3                      Targets Group for Solid Elements Type

Includes 2D or 3D forces, stresses and strains for a solid elements type.

Table 6.5-3 Solid Elements Type

Item

Component

Type

Label

S

X

MIN

SX-

S

Y

MIN

SY-

S

Z

MIN

SZ-

S

XY

MIN

SXY-

S

YZ

MIN

SYZ-

S

XZ

MIN

SXZ-

EPEL

X

MIN

EPELX-

EPEL

Y

MIN

EPELY-

EPEL

Z

MIN

EPELZ-

EPEL

XY

MIN

EPELXY-

EPEL

YZ

MIN

EPELYZ-

EPEL

XZ

MIN

EPELXZ-

S

X

MAX

SX+

S

Y

MAX

SY+

S

Z

MAX

SZ+

S

XY

MAX

SXY+

S

YZ

MAX

SYZ+

S

XZ

MAX

SXZ+

EPEL

X

MAX

EPELX+

EPEL

Y

MAX

EPELY+

EPEL

Z

MAX

EPELZ+

EPEL

XY

MAX

EPELXY+

EPEL

YZ

MAX

EPELYZ+

EPEL

XZ

MAX

EPELXZ+

S

X

ABS

SX*

S

Y

ABS

SY*

S

Z

ABS

SZ*

S

XY

ABS

SXY*

S

YZ

ABS

SYZ*

S

XZ

ABS

SXZ*

EPEL

X

ABS

EPELX*

EPEL

Y

ABS

EPELY*

EPEL

Z

ABS

EPELZ*

EPEL

XY

ABS

EPELXY*

EPEL

YZ

ABS

EPELYZ*

EPEL

XZ

ABS

EPELXZ*

6.5.4                      Targets Group for Axial Symmetric Shell Elements Type

Includes forces, moments, stresses and strains at axial symmetric shell elements.

Table 6.5-4 Axis Symmetric Shell Elements Type

Item

Component

Type

Label

F

X

MIN

FX-

F

Y

MIN

FY-

F

Z

MIN

FZ-

M

Z

MIN

MZ-

S

MT

MIN

SMT-

S

THKT

MIN

STHKT-

S

HT

MIN

SHT-

S

MHT

MIN

SMHT-

S

MM

MIN

SMM-

S

THKM

MIN

STHKM-

S

HM

MIN

SHM-

S

MHM

MIN

SMHM-

S

MB

MIN

SMB-

S

THKB

MIN

STHKB-

S

HB

MIN

SHB-

S

MHB

MIN

SMHB-

EPEL

MT

MIN

EPELMT-

EPEL

THKT

MIN

EPELTHKT-

EPEL

HT

MIN

EPELHT-

EPEL

MHT

MIN

EPELMHT-

EPEL

MM

MIN

EPELMM-

EPEL

THKM

MIN

EPELTHKM-

EPEL

HM

MIN

EPELHM-

EPEL

MHM

MIN

EPELMHM-

EPEL

MB

MIN

EPELMB-

EPEL

THKB

MIN

EPELTHKB-

EPEL

HB

MIN

EPELHB-

EPEL

MHB

MIN

EPELMHB-

F

X

MAX

FX+

F

Y

MAX

FY+

F

Z

MAX

FZ+

M

Z

MAX

MZ+

S

MT

MAX

SMT+

S

THKT

MAX

STHKT+

S

HT

MAX

SHT+

S

MHT

MAX

SMHT+

S

MM

MAX

SMM+

S

THKM

MAX

STHKM+

S

HM

MAX

SHM+

S

MHM

MAX

SMHM+

S

MB

MAX

SMB+

S

THKB

MAX

STHKB+

S

HB

MAX

SHB+

S

MHB

MAX

SMHB+

EPEL

MT

MAX

EPELMT+

EPEL

THKT

MAX

EPELTHKT+

EPEL

HT

MAX

EPELHT+

EPEL

MHT

MAX

EPELMHT+

EPEL

MM

MAX

EPELMM+

EPEL

THKM

MAX

EPELTHKM+

EPEL

HM

MAX

EPELHM+

EPEL

MHM

MAX

EPELMHM+

EPEL

MB

MAX

EPELMB+

EPEL

THKB

MAX

EPELTHKB+

EPEL

HB

MAX

EPELHB+

EPEL

MHB

MAX

EPELMHB+

 

 

 

 

F

X

ABS

FX*

F

Y

ABS

FY*

F

Z

ABS

FZ*

M

Z

ABS

MZ*

S

MT

ABS

SMT*

S

THKT

ABS

STHKT*

S

HT

ABS

SHT*

S

MHT

ABS

SMHT*

S

MM

ABS

SMM*

S

THKM

ABS

STHKM*

S

HM

ABS

SHM*

S

MHM

ABS

SMHM*

S

MB

ABS

SMB*

S

THKB

ABS

STHKB*

S

HB

ABS

SHB*

S

MHB

ABS

SMHB*

EPEL

MT

ABS

EPELMT*

EPEL

THKT

ABS

EPELTHKT*

EPEL

HT

ABS

EPELHT*

EPEL

MHT

ABS

EPELMHT*

EPEL

MM

ABS

EPELMM*

EPEL

THKM

ABS

EPELTHKM*

EPEL

HM

ABS

EPELHM*

EPEL

MHM

ABS

EPELMHM*

EPEL

MB

ABS

EPELMB*

EPEL

THKB

ABS

EPELTHKB*

EPEL

HB

ABS

EPELHB*

EPEL

MHB

ABS

EPELMHB*

6.5.5                      Targets Group for Displacements

Includes displacements and rotations at the nodes.

Table 6.5-5 Displacements

Item

Component

Type

Label

U

X

MIN

UX-

U

Y

MIN

UY-

U

Z

MIN

UZ-

ROT

X

MIN

ROTX-

ROT

Y

MIN

ROTY-

ROT

Z

MIN

ROTZ-

U

X

MAX

UX+

U

Y

MAX

UY+

U

Z

MAX

UZ+

ROT

X

MAX

ROTX+

ROT

Y

MAX

ROTY+

ROT

Z

MAX

ROTZ+

U

X

ABS

UX*

U

Y

ABS

UY*

U

Z

ABS

UZ*

ROT

X

ABS

ROTX*

ROT

Y

ABS

ROTY*

ROT

Z

ABS

ROTZ*

6.5.6                      Targets Group for Nodal Reactions

Includes forces and moments as reactions at the nodes.

Table 6.5-5 Reactions

Item

Component

Type

Label

F

X

MIN

FX-

F

Y

MIN

FY-

F

Z

MIN

FZ-

M

X

MIN

MX-

M

Y

MIN

MY-

M

Z

MIN

MZ-

F

X

MAX

FX+

F

Y

MAX

FY+

F

Z

MAX

FZ+

M

X

MAX

MX+

M

Y

MAX

MY+

M

Z

MAX

MZ+

F

X

ABS

FX*

F

Y

ABS

FY*

F

Z

ABS

FZ*

M

X

ABS

MX*

M

Y

ABS

MY*

M

Z

ABS

MZ*

6.5.7                      Targets Group for Cross Sections

 

This group includes forces, moments, stresses, and strains at the points of the section calculated by CivilFEM and is filed in the CivilFEM results file (.RCV).

Given that the number of points in a section is variable and may grow indefinitely, the number of targets is limited to 6 for forces and moments, 14 for stresses and 14 for strains. For the last two cases, the target refers to a point and a component of the stress or strain at that point, defined by the user (see ~TRGUPT command).

However, concomitance is established for all data composed of the forces and moments of the section and all the components of the stresses and strains at every point of the section.

The user can define a set of stress or strain points, represented in the following table by PT1, PT2 … PTn.

Table 6.5-7 Cross Sections

 

Item

Component

Type

Label

F

X

MIN

FX-

F

Y

MIN

FY-

F

Z

MIN

FZ-

M

X

MIN

MX-

M

Y

MIN

MY-

M

Z

MIN

MZ-

SS

PT1

MIN

SSPT1-

SS

PT2

MIN

SSPT2-

SS

PT3

MIN

SSPT3-

SS

PT4

MIN

SSPT4-

SS

PT5

MIN

SSPT5-

SS

PT6

MIN

SSPT6-

SS

PT7

MIN

SSPT7-

SS

PT8

MIN

SSPT8-

SS

PT9

MIN

SSPT9-

SS

PT10

MIN

SSPT10-

SS

PT11

MIN

SSPT11-

SS

PT12

MIN

SSPT12-

SS

PT13

MIN

SSPT13-

SS

PT14

MIN

SSPT14-

EP

PT1

MIN

EPPT1-

EP

PT2

MIN

EPPT2-

EP

PT3

MIN

EPPT3-

EP

PT4

MIN

EPPT4-

EP

PT5

MIN

EPPT5-

EP

PT6

MIN

EPPT6-

EP

PT7

MIN

EPPT7-

EP

PT8

MIN

EPPT8-

EP

PT9

MIN

EPPT9-

EP

PT10

MIN

EPPT10-

EP

PT11

MIN

EPPT11-

EP

PT12

MIN

EPPT12-

EP

PT13

MIN

EPPT13-

EP

PT14

MIN

EPPT14-

F

X

MAX

FX+

F

Y

MAX

FY+

F

Z

MAX

FZ+

M

X

MAX

MX+

M

Y

MAX

MY+

M

Z

MAX

MZ+

SS

PT1

MAX

SSPT1+

SS

PT2

MAX

SSPT2+

SS

PT3

MAX

SSPT3+

SS

PT4

MAX

SSPT4+

SS

PT5

MAX

SSPT5+

SS

PT6

MAX

SSPT6+

SS

PT7

MAX

SSPT7+

SS

PT8

MAX

SSPT8+

SS

PT9

MAX

SSPT9+

SS

PT10

MAX

SSPT10+

SS

PT11

MAX

SSPT11+

SS

PT12

MAX

SSP12+

SS

PT13

MAX

SSPT13+

SS

PT14

MAX

SSPT14+

EP

PT1

MAX

EPT1+

EP

PT2

MAX

EPT2+

EP

PT3

MAX

EPT3+

EP

PT4

MAX

EPT4+

EP

PT5

MAX

EPPT5+

EP

PT6

MAX

EPPT6+

EP

PT7

MAX

EPPT7+

EP

PT8

MAX

EPPT8+

EP

PT9

MAX

EPPT9+

EP

PT10

MAX

EPPT10+

EP

PT11

MAX

EPPT11+

EP

PT12

MAX

EPPT12+

EP

PT13

MAX

EPPT13+

EP

PT14

MAX

EPPT14+

F

X

ABS

FX*

F

Y

ABS

FY*

F

Z

ABS

FZ*

M

X

ABS

MX*

M

Y

ABS

MY*

M

Z

ABS

MZ*

SS

PT1

ABS

SSPT1*

SS

PT2

ABS

SSPT2*

SS

PT3

ABS

SSPT3*

SS

PT4

ABS

SSPT4*

SS

PT5

ABS

SSPT5*

SS

PT6

ABS

SSPT6*

SS

PT7

ABS

SSPT7*

SS

PT8

ABS

SSPT8*

SS

PT9

ABS

SSPT9*

SS

PT10

ABS

SSPT10*

SS

PT11

ABS

SSPT11*

SS

PT12

ABS

SSP12*

SS

PT13

ABS

SSPT13*

SS

PT14

ABS

SSPT14*

EP

PT1

ABS

EPT1*

EP

PT2

ABS

EPT2*

EP

PT3

ABS

EPT3*

EP

PT4

ABS

EPT4*

EP

PT5

ABS

EPPT5*

EP

PT6

ABS

EPPT6*

EP

PT7

ABS

EPPT7*

EP

PT8

ABS

EPPT8*

EP

PT9

ABS

EPPT9*

EP

PT10

ABS

EPPT10*

EP

PT11

ABS

EPPT11*

EP

PT12

ABS

EPPT12*

EP

PT13

ABS

EPPT13*

EP

PT14

ABS

EPPT14*

 

6.5.8                      Targets Group for Shell Vertices

 

They include forces, moments, stresses and strains obtained by CivilFEM in the shell vertices and stored in the CivilFEM results file (.RCV).

 

Table 6.5-8 Shell elements

 

Item

Component

Type

Label

T

X

MIN

TX-

T

Y

MIN

TY-

T

XY

MIN

TXY-

M

X

MIN

MX-

M

Y

MIN

MY-

M

XY

MIN

MXY-

N

X

MIN

NX-

N

Y

MIN

NY-

S

XT

MIN

SXT-

S

YT

MIN

SYT-

S

ZT

MIN

SZT-

S

XYT

MIN

SXYT-

S

YZT

MIN

SYZT-

S

XZT

MIN

SXZT-

S

XB

MIN

SXB-

S

YB

MIN

SYB-

S

ZB

MIN

SZB-

S

XYB

MIN

SXYB-

S

YZB

MIN

SYZB-

S

XZB

MIN

SXZB-

EPEL

XT

MIN

EPELXT-

EPEL

YT

MIN

EPELYT-

EPEL

ZT

MIN

EPELZT-

EPEL

XYT

MIN

EPELXYT-

EPEL

YZT

MIN

EPELYZT-

EPEL

XZT

MIN

EPELXZT-

EPEL

XB

MIN

EPELXB-

EPEL

YB

MIN

EPELYB-

EPEL

ZB

MIN

EPELZB-

EPEL

XYB

MIN

EPELXYB-

EPEL

YZB

MIN

EPELYZB-

EPEL

XZB

MIN

EPELXZB-

T

X

MAX

TX+

T

Y

MAX

TY+

T

XY

MAX

TXY+

M

X

MAX

MX+

M

Y

MAX

MY+

M

XY

MAX

MXY+

N

X

MAX

NX+

N

Y

MAX

NY+

S

XT

MAX

SXT+

S

YT

MAX

SYT+

S

ZT

MAX

SZT+

S

XYT

MAX

SXYT+

S

YZT

MAX

SYZT+

S

XZT

MAX

SXZT+

S

XB

MAX

SXB+

S

YB

MAX

SYB+

S

ZB

MAX

SZB+

S

XYB

MAX

SXYB+

S

YZB

MAX

SYZB+

S

XZB

MAX

SXZB+

EPEL

XT

MAX

EPELXT+

EPEL

YT

MAX

EPELYT+

EPEL

ZT

MAX

EPELZT+

EPEL

XYT

MAX

EPELXYT+

EPEL

YZT

MAX

EPELYZT+

EPEL

XZT

MAX

EPELXZT+

EPEL

XB

MAX

EPELXB+

EPEL

YB

MAX

EPELYB+

EPEL

ZB

MAX

EPELZB+

EPEL

XYB

MAX

EPELXYB+

EPEL

YZB

MAX

EPELYZB+

EPEL

XZB

MAX

EPELXZB+

T

X

ABS

TX*

T

Y

ABS

TY*

T

XY

ABS

TXY*

M

X

ABS

MX*

M

Y

ABS

MY*

M

XY

ABS

MXY*

N

X

ABS

NX*

N

Y

ABS

NY*

S

XT

ABS

SXT*

S

YT

ABS

SYT*

S

ZT

ABS

SZT*

S

XYT

ABS

SXYT*

S

YZT

ABS

SYZT*

S

XZT

ABS

SXZT*

S

XB

ABS

SXB*

S

YB

ABS

SYB*

S

ZB

ABS

SZB*

S

XYB

ABS

SXYB*

S

YZB

ABS

SYZB*

S

XZB

ABS

SXZB*

EPEL

XT

ABS

EPELXT*

EPEL

YT

ABS

EPELYT*

EPEL

ZT

ABS

EPELZT*

EPEL

XYT

ABS

EPELXYT*

EPEL

YZT

ABS

EPELYZT*

EPEL

XZT

ABS

EPELXZT*

EPEL

XB

ABS

EPELXB*

EPEL

YB

ABS

EPELYB*

EPEL

ZB

ABS

EPELZB*

EPEL

XYB

ABS

EPELXYB*

EPEL

YZB

ABS

EPELYZB*

EPEL

XZB

ABS

EPELXZB*

 

6.6                       Envelopes

The data stored in the CivilFEM results file are stored in two different types of data blocks: blocks of stresses, forces, moments and strains and blocks of alternatives.

Data blocks of stresses, forces, moments and strains are associated to an ANSYS DataSet and are obtained and stored in solution time. The content of these blocks is similar and their structure is always the same.

Alternative blocks differ from each other in their content because their content varies depending on the process (checking, design, etc.) that generated the alternative. The data are obtained in postprocessor time, storing the data of forces, moments, stresses and strains from the corresponding blocks. Each block of forces, moments, stresses and strains may generate one or more alternative blocks (checking according to different codes or changing various parameters). 

The utilities of the combination module are ONLY applied to the blocks of stresses, forces, moments and strains associated to an ANSYS DataSet.

The utility ENVELOPE has been developed for alternative blocks. This utility is included in the generation and usage of the file *.RCV which allows the creation of other alternatives as envelope of others previously obtained. Envelopes have to be homogeneous; specifically, they must be obtained by the application of the same code and process to the same model. The resulting alternative will be homogeneous with the previous ones, with a similar identification and the same commands for reading, drawing and representation.

There are 3 types of envelopes:

·         Maximum values envelope

·         Minimum values envelope

·         Maximum absolute value envelope.

An envelope of several alternatives consists of initial envelopes; these envelopes contain the set of minimum, maximum or absolute maximum values (depending on type) of data taken from all of the initial alternatives.

6.7                       Concomitance at Load and Model Level

The coefficients that are used to multiply the Start States of a combination that achieve a certain Target at a specific node of the structure can be obtained with the ~CMBINQ command.  This command displays a list of the coefficients utilized in each one of the Start States of the combination rule. It is also possible for this command to display the coefficients of Start States in a nested combination.

With this command, the TARGET combined result as well as any concomitant values of the TARGET group can be determined.

It will allow the user to define the load state that will determine the requested Target by calculating the coefficients of each start state of the specified combination rule. Likewise, every start state coefficient from all the combinations will be calculated in the same way.

For the specific combination rule selected, the concomitant loads in the model are stored in the ANSYS and CivilFEM databases. The results for this load step will be available until a new Data Set is specified by means of the ~CFSET or ~CMBDAT commands. The results from the ~CMBINQ command cannot be used for checking or dimensioning operations conforming to codes.

6.8                       Comments about Beam188 and Beam189 Elements

The ANSYS commands PLDISP or PLNSOL, U plot the deformed shape of a beam structure, beginning with the nodal displacements for all types of beam elements; the plot will display the linear structure with its deformed shape.

If the option /ESHAPE,1 is activated (plot the section shape), ANSYS converts the linear elements into a rectangular section, taking its characteristics from the real constants. This section remains undeformed throughout the element; except, with BEAM188 and BEAM189 elements, ANSYS contains additional information such as the section shape, cross section cells (subdivision) and output information at the section nodes. Due to this additional information, ANSYS can calculate and plot the element’s deformed shape as well as the deformed shape at the section’s internal nodes for these two element types.

ANSYS stores the information about nodal displacements and section strains in the results file (file.RST).

When combinations are performed in CivilFEM, a results file (file.CMB) is generated with the same format as the ANSYS results file (file.RST); ANSYS can read this CMB file as if it were an RST file, taking all the required postprocessing information from this file, such as the deformed shape of the structure.  

As in CivilFEM, after performing the combinations, ANSYS establishes the concomitance at the group level (as discussed previously); when performing a combination for a target of displacements, concomitant data will be the remaining displacements and rotations, but not the section strains which will be left as zero.

For this reason, if the commands PLDISP and PLNSOL,U are applied with the option /ESHAPE,1 on a structure with Beam188 and Beam189 elements, the program will not plot the deformed shape correctly for a combined result of a displacement target. Nevertheless it is still  possible to list the correct results.

To plot the correct results, it is necessary to use the option /ESHAPE,0.

 

6.9                       Start State Combinations with Prestressing Tendons

If the start states used within combinations contain results from a prestressed concrete structure, consult the corresponding chapter of the Advanced Prestressed Concrete Module documentation for further considerations.

 

6.10                 Calculation of All Possible Load Cases

In some cases it may be useful to obtain all the load cases that a certain combination rule can generate. The process is as follows:

  • Define combination rules. As seen in Chapter 6.4.
  • Perform combinations by using the ~LINCMB command.
  • Review results.

The load cases are obtained by linearly by combining the initial load steps, as defined in the combination rules, with the desired coefficients.

These new load cases are stored in the RCV and RST files (no CMB or CVMB files are created), after the initial load cases. To postprocess these load cases, it is necessary to read them first, just as any other load case (~CFSET command).

A list of all the newly generated load cases can be obtained with the ~LINLST command. This list will provide information about the combination rule of each load case, the initial load cases and the coefficients used (only available if the RCV file has been created).

 

Note:

It is important to keep in mind that Load Combinations can result in a very high number of load cases.

The calculation of all possible load cases is not recommended for loads generated by moving vehicles or arbitrary surface loads. For example, a combination with 18 different locations of a load, using a COMPATIBLE combination type, would result in 218 = 262144 different load cases.

Combinations with targets, as explained in the previous chapters, are more suitable for defined load combinations that may result in many load cases, as in the case of moving vehicles or arbitrary surface loads.

 

6.11                 Automatic load combinations for standards

There is a simple and powerful tool in CivilFEM to obtain all the necessary combinations of actions for the Ultimate Limit States (ULS) and Service Limit States (SLS) with the following standards:

·         Eurocode

·         ASCE 7-05

·         ASCE 7-10

Once all the load steps have been solved (it is highly recommended to have titles in each of them to identify each data set) in solution, the user can use the Code Combination window located here:
Main Menu > CIVIL Postprocessor > Code Combination

Once within the window, the user will be able to generate all the combinations according to the selected standard.

See help of ~CCMB command.

6.11.1                  Eurocode Combinations

If Eurocode is selected as the active code in the lower left corner, it will be possible to proceed to the generation of the combinations of actions according to the Eurocode, including the coefficients for simultaneous actions:

·         ULS: Permanent actions, persistent or transient; Accidental and Seismic.

·         SLS: Characteristic combination, unlikely or rare; frequent and quasi-permanent.

From the Loads tab, the actions are entered with their corresponding editable coefficients γ, ψ (favorable/unfavourable effect partials and simultaneous actions). User can add as many loads as needed.

 

 

Incompatibilities between actions may occur:

1.    Two loads are incompatible with each other when it cannot be the case that the two appear in any combination together.

2.    A dominant load is incompatible with another concomitant when it is not possible for the two to appear in any combination together.

In the same way, the concomitance between actions can be defined. All the charges that belong to a group of charges will appear together in the combinations, being all at the same time either dominant or concomitant.

 

Once the loads and the incompatibilities between them have been defined, the combinations can be calculated. In this section you can choose the types of combination that you want the program to carry out (ULS and SLS).

 

 

It will be possible to proceed with the previous generation of the combinations with the Generate Preview button.

The program warns that a high number of combinations can be generated and that extra resources from both CivilFEM and the computer can be consumed.

CivilFEM will create the combinations (with their corresponding new load steps) inside the results files (RST and RCV).

 

 

The list of combinations can be exported to a word file.

It is also available to save the configuration of actions performed within the window to an external file.

In the same way, the user will be able to access the APDL command lines that generate what has been done within the window in a script.

 

6.11.2                  ASCE combinations of loads

If ASCE standards are chosen for the generation of load combinations then the process is simplified into two groups:

1.    Design according to Strength Design.

2.    Design according to Allowable Stress Design.

The selection of loads is the same as with the Eurocode, but here the type of load is selected according to dropdown lists: Dead, Live, Roof Live, Wind, Seismic, Rain, Snow.

 

 

The combining factored loads are automatically defined according to Basic Combinations of Strength Design or/and Allowable Stress Design.

 

The list of combinations can be exported to a word file.

It is also available to save the configuration of actions performed within the window to an external file.

In the same way, the user will be able to access the APDL command lines that generate what has been done within the window in a script.