7.4.11.2. Output Node(FFlex)

The lists of nodes include a result set about each node as position, velocity, acceleration, strain and stress.

Output

Plot Content

Outputs

Node

Pos_

Position and Z-X-Z euler angles of the node

Vel_

Velocity of the node. The translational velocity is measured in the inertia reference frame. The angular velocity is measured in the reference frame of node

Acc_

Acceleration of the node. The translational acceleration is measured in the inertia reference frame. The angular acceleration is measured in the reference frame of node.

EX,EY,EZ ,EXY,EYZ,EZY

Strain tensor measured in the inertia reference frame.

E1,E2,E3

Principal Strain.

E1X, E1Y, E1Z, E2X, E2Y, E2Z, E3X, E3Y, E3Z,

Vector of Principal Strain. These values are Eigenvector of Principal Strain. It can be calculated like following.

\(\begin{aligned} & \left[ \begin{matrix} E1X \\ E1Y \\ E1Y \\ \end{matrix} \right]=E1\left[ \begin{matrix} EV_{X}^{1} \\ EV_{Y}^{1} \\ EV_{Z}^{1} \\ \end{matrix} \right],\left[ \begin{matrix} E2X \\ E2Y \\ E2Y \\ \end{matrix} \right]=E2\left[ \begin{matrix} EV_{X}^{2} \\ EV_{Y}^{2} \\ EV_{Z}^{2} \\ \end{matrix} \right],\left[ \begin{matrix} E3X \\ E3Y \\ E3Y \\ \end{matrix} \right]=E3\left[ \begin{matrix} EV_{X}^{3} \\ EV_{Y}^{3} \\ EV_{Z}^{3} \\ \end{matrix} \right] \\ & EV:EigenVectors(Strain) \\ & E1,E2,E3:Eigenvalues(Strain) \\ \end{aligned}\)

(These components are written when the output option is checked. Output Principal Component of Stress/Strain can be found under dialog where Home-Setting-Flexibility-Flexible tab.)

EINT

Intensity Strain.

EMISES

Von-Mises Strain.

_T, _P, _E, _THERMAL

_E is the elastic strain.

_P is the plastic strain.

_T is the total strain.

_Thermal is the thermal strain.

SX,SY,SZ ,SXY,SYZ,SZY

Stress tensor measured in the inertia reference frame.

S1,S2,S3

Principal Stress.

S1X, S1Y, S1Z, S2X, S2Y, S2Z, S3X, S3Y, S3Z,

Vector of Principal Stress.

\(\begin{aligned} & \left[ \begin{matrix} S1X \\ S1Y \\ S1Y \\ \end{matrix} \right]=S1\left[ \begin{matrix} EV_{X}^{1} \\ EV_{Y}^{1} \\ EV_{Z}^{1} \\ \end{matrix} \right],\left[ \begin{matrix} S2X \\ S2Y \\ S2Y \\ \end{matrix} \right]=S2\left[ \begin{matrix} EV_{X}^{2} \\ EV_{Y}^{2} \\ EV_{Z}^{2} \\ \end{matrix} \right],\left[ \begin{matrix} S3X \\ S3Y \\ S3Y \\ \end{matrix} \right]=S3\left[ \begin{matrix} EV_{X}^{3} \\ EV_{Y}^{3} \\ EV_{Z}^{3} \\ \end{matrix} \right] \\ & EV:EigenVectors(Stress) \\ & S1,S2,S3:Eigenvalues(Stress) \\ \end{aligned}\)

(These components are written when the output option is checked. Output Principal Component of Stress/Strain can be found under dialog where Home-Setting-Flexibility-Flexible tab.)

SINT

Intensity Stress.

SMISES

Von-Mises Stress.

  • Report Data Combination Map.

Table 7.4 Base components of Strain and Stress

\(\mathbf{\epsilon}\)

\(\mathbf{\sigma}\)

EX

SX

EY

SY

EZ

SZ

EXY

SXY

EYZ

SYZ

EZX

SZX

E1

S1

E2

S2

E3

S3

E1X

S1X

E1Y

S1Y

E1Z

S1Z

E2X

S2X

E2Y

S2Y

E2Z

S2Z

E3X

S3X

E3Y

S3Y

E3Z

S3Z

EINT

SINT

EVON

SVON

Table 7.5 Strain and Stress Data

Elastic

Elastic+Thermal

Plastic

Plastic+Thermal

GENERAL

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

SHELL

TOP

TOP

TOP

TOP

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

BOTTOM

BOTTOM

BOTTOM

BOTTOM

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

BEAM

MAX_DISTANCE

MAX_DISTANCE

MAX_DISTANCE

MAX_DISTANCE

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

C

C

C

C

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

D

D

D

D

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

E

E

E

E

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

F

F

F

F

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

Max_Mises

Max_Mises

Max_Mises

Max_Mises

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Total}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Elastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Plastic}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\epsilon}_{Thermal}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

\(\mathbf{\sigma}_{Total}\)

  • The output node can be defined which belong to RBE or RBE3. In this case, RPLT data should be same as basic data.

  • One output node can belong to many types of element. In this case, the output data is separated by element type. (BEAM / SHELL / SOLID)