STRAIN

 

The STRAIN function returns the strain acting on a designated node on a flexible body.

 

Format

Using reference marker

 

Using 3 reference nodes

 

Arguments definition

Node ID

Node number, including the names of the FFlex or RFlex Body, or argument number for the nodes to calculated for the strain value

Type

Symbol that indicates the type of strain to measure

Strain

Type

Discription

Basic strain

X

x direction from x face

Y

y direction from y face

Z

z direction from z face

XY

y direction from x face

YZ

z direction from y face

ZX

z direction from z face

Principal strain

E1

First principal

E2

Second principal

E3

Third principal

Intensity

INT

 

Von-mises strain

VON

 

Setting Reference Frame

RMarker

The name or argument number of the standard marker for direction to be measured

3 reference nodes

The name or argument number of the 3 reference nodes which define reference frame to be measured

Position 

Recovery Postion for FFlex output node

 

Type

Meaning of Caculated data

TOP

SOLID + SHELL TOP + BEAM MAX DIST

BOTTOM

SOLID + SHELL BOTTOM + BEAM MAX DIST

MD

SOLID + SHELL TOP + BEAM MAX DIST

C

SOLID + SHELL TOP + BEAM C

D

SOLID + SHELL TOP + BEAM D

E

SOLID + SHELL TOP + BEAM E

F

SOLID + SHELL TOP + BEAM F

MV

SOLID + SHELL TOP + BEAM MAX VMISES

TOP_MD

SOLID + SHELL TOP + BEAM MAX DIST

TOP_C

SOLID + SHELL TOP + BEAM C

TOP_D

SOLID + SHELL TOP + BEAM D

TOP_E

SOLID + SHELL TOP + BEAM E

TOP_F

SOLID + SHELL TOP + BEAM F

TOP_MV

SOLID + SHELL TOP + BEAM MAX VMISES

BOTTOM_MD

SOLID + SHELL BOTTOM + BEAM MAX DIST

BOTTOM_C

SOLID + SHELL BOTTOM + BEAM C

BOTTOM_D

SOLID + SHELL BOTTOM + BEAM D

BOTTOM_E

SOLID + SHELL BOTTOM + BEAM E

BOTTOM_F

SOLID + SHELL BOTTOM + BEAM F

BOTTOM_MV

SOLID + SHELL TOP + BEAM MAX VMISES

ONLY_TOP

SHELL TOP

ONLY_BOTTOM

SHELL BOTTOM

ONLY_MD

BEAM MAX DIST

ONLY_C

BEAM C

ONLY_D

BEAM D

ONLY_E

BEAM E

ONLY_F

BEAM F

ONLY_MV

BEAM MAX VMISES

ONLY_SOLID

SOLID

 

If the recovery position is not specified, the default value is the TOP for shell and MD for beam.

If the RFlex body has only one stress shape, this argument is ignored.

 

Reference Frame defined by 3 reference nodes

 

Figure 1 Definition of 3 nodal points reference frame

 

The reference frame defined by 3 nodal points is like above figure. X direction is parallel to the vector from reference node1 to reference node2 and Z direction is normal to the face which consist of 3 nodal points.

 

Example

STRAIN(Body1_FE.node1,X,Ground.InertiaMarker)

STRAIN(1,VON,2) < Argument: (1) Body1_FE.node1 (2) Ground.InertiaMarker >

 

Figure 2  Example Expression using Strain function using RM

 

STRAIN(1,VON,2,3,4) < Argument: (1) Body1_FE.node50588 (2) Body1_FE.node50578 (3) Body1_FE.node50579 (4) Body1_FE.node50562 >

 

Figure 3  Example Expression using Strain function using 3 reference nodes

 

Note

The strain expression must not be used to apply the dependent force. Only the expression is used in the post procedure.

In order to see the strain result for non-output nodes in Scope Expression, all component such as EX, EY etc should be included in output files.