| 3000
|
BAR MOMENT END A-Z PLANE 1
|
Bar element bending moment at end A about element z-direction. Controlled by
FORCE Case Control command.
|
| 3001
|
BAR MOMENT END A-Y PLANE 2
|
Bar element bending moment at end A about element y-direction. Controlled by FORCE Case Control command.
|
| 3002
|
BAR MOMENT END B-Z PLANE 1
|
Bar element bending moment at end B about element z-direction. Controlled by FORCE Case Control command.
|
| 3003
|
BAR MOMENT END B-Y PLANE 2
|
Bar element bending moment at end B about element y-direction. Controlled by FORCE Case Control command.
|
| 3004
|
BAR FORCE END A-Y PLANE 1
|
Bar element transverse shear force at end A in element y-direction. Controlled by FORCE Case Control command.
|
| 3005
|
BAR FORCE END A-Z PLANE 2
|
Bar element transverse shear force at end A in element z-direction. Controlled by FORCE Case Control command.
|
| 3006
|
BAR FORCE END B-Y PLANE 1
|
Bar element transverse shear force at end B in element y-direction. Controlled by FORCE Case Control command.
|
| 3007
|
BAR FORCE END B-Z PLANE 2
|
Bar element transverse shear force at end B in element z-direction. Controlled by FORCE Case Control command.
|
| 3008
|
BAR FORCE END A-X
|
Bar element axial force at end A in element x-direction. Controlled by FORCE Case Control command.
|
| 3009
|
BAR FORCE END B-X
|
Bar element axial force at end B in element x-direction. Controlled by FORCE Case Control command.
|
| 3010
|
BAR MOMENT END A-X
|
Bar element torque at end A about element x-direction. Controlled by FORCE Case Control command.
|
| 3011
|
BAR MOMENT END B-X
|
Bar element torque at end B about element x-direction. Controlled by FORCE Case Control command.
|
| 3075
|
BAR STRESS END A POINT C
|
Bar element stress at end A, stress recovery point C. For bar elements this stress will only include bending contributions. Controlled by
STRESS Case Control command.
|
| 3076
|
BAR STRESS END A POINT D
|
Bar element stress at end A, stress recovery point D. For bar elements this stress will only include bending contributions. Controlled by STRESS Case Control command.
|
| 3077
|
BAR STRESS END A POINT E
|
Bar element stress at end A, stress recovery point E. For bar elements this stress will only include bending contributions. Controlled by STRESS Case Control command.
|
| 3078
|
BAR STRESS END A POINT F
|
Bar element stress at end A, stress recovery point F. For bar elements this stress will only include bending contributions. Controlled by STRESS Case Control command.
|
| 3083
|
BAR STRESS END B POINT C
|
Bar element stress at end B, stress recovery point C. For bar elements this stress will only include bending contributions. Controlled by STRESS Case Control command.
|
| 3084
|
BAR STRESS END B POINT D
|
Bar element stress at end B, stress recovery point D. For bar elements this stress will only include bending contributions. Controlled by STRESS Case Control command.
|
| 3085
|
BAR STRESS END B POINT E
|
Bar element stress at end B, stress recovery point E. For bar elements this stress will only include bending contributions. Controlled by STRESS Case Control command.
|
| 3086
|
BAR STRESS END B POINT F
|
Bar element stress at end B, stress recovery point F. For bar elements this stress will only include bending contributions. Controlled by STRESS Case Control command.
|
| 3107
|
BAR STRESS END A-AXIAL
|
Bar element axial stress at end A. Controlled by STRESS Case Control command.
|
| 3108
|
BAR STRESS END B-AXIAL
|
Bar element axial stress at end B. Controlled by STRESS Case Control command.
|
| 3109
|
BAR STRESS END A-MAX
|
Bar element maximum stress (bending and axial) for all points at end A. Controlled by
STRESS Case Control command.
|
| 3110
|
BAR STRESS END A-MIN
|
Bar element minimum stress (bending and axial) for all points at end A. Controlled by STRESS Case Control command.
|
| 3111
|
BAR STRESS END B-MAX
|
Bar element maximum stress (bending and axial) for all points at end B. Controlled by STRESS Case Control command.
|
| 3112
|
BAR STRESS END B-MIN
|
Bar element minimum stress (bending and axial) for all points at end B. Controlled by STRESS Case Control command.
|
| 3195
|
BAR VON MISES STRESS
|
Bar element von Mises stress. Controlled by STRESS Case Control command.
|
| 3293
|
BAR EQUIVALENT STRESS
|
For .out file outputs, this represents the bar element nonlinear equivalent axial stress (material nonlinear solutions) or axial stress (linear solutions). For .fno file outputs, this represents the maximum bar element stress (both axial and bending stresses). Note that for prestress solutions, regardless of PARAM,
ADDPRESTRESS setting, equivalent stress will not include prestress contribution. Controlled by
STRESS or
STRAIN Case Control commands (linear solutions) and
NLSTRESS Case Control command (nonlinear solutions).
|
| 3293
|
BAR VON MISES STRESS-BENDING
|
Bar element von Mises stress computed without membrane stress contribution. Controlled by STRESS or STRAIN Case Control commands and PARAM,
EQVSTRESSTYPE setting.
|
| 3293
|
BAR VON MISES STRESS-MEMBRANE
|
Bar element von Mises stress computed without bending stress contribution. Controlled by STRESS or STRAIN Case Control commands and PARAM, EQVSTRESSTYPE setting.
|
| 3294
|
BAR EFFECTIVE STRAIN-ELASTIC
|
Bar element effective axial strain. Note that for prestress solutions, regardless of PARAM, ADDPRESTRESS setting, effective strain will not include prestress contribution. Controlled by STRESS or STRAIN Case Control commands.
|
| 3294
|
BAR EFFECTIVE STRAIN-PLASTIC/NONLINEAR ELASTIC
|
Bar element effective strain (nonlinear elastic material) or plastic strain (elastic-plastic material). Controlled by NLSTRESS Case Control command.
|
| 3295
|
BAR EFFECTIVE STRAIN-CREEP
|
Bar element effective creep strain. Controlled by NLSTRESS Case Control command.
|
| 3440
|
BAR MAX STRESS
|
Bar element maximum stress (bending and axial) for all points at end A and B. Controlled by STRESS Case Control command.
|
| 3441
|
BAR MIN STRESS
|
Bar element minimum stress (bending and axial) for all points at end A and B. Controlled by STRESS Case Control command.
|
| 3442
|
BAR LOCATION A
|
Bar element end A location.
|
| 3443
|
BAR LOCATION B
|
Bar element end B location.
|
| 3481
|
BAR STATUS
|
Solution and option dependent. In modal summation solutions (DDAM) STATUS, is the mode number with the maximum response in the NRL summation. In solutions where a factor of safety calculation method has been defined on a
MAT1 entry, STATUS is the factor of safety.
|
| 3575
|
BAR STRAIN END A POINT C
|
Bar element strain at end A, strain recovery point C. For bar elements this stress will only include bending contributions. Controlled by
STRAIN Case Control command.
|
| 3576
|
BAR STRAIN END A POINT D
|
Bar element strain at end A, strain recovery point D. For bar elements this strain will only include bending contributions. Controlled by STRAIN Case Control command.
|
| 3577
|
BAR STRAIN END A POINT E
|
Bar element strain at end A, strain recovery point E. For bar elements this strain will only include bending contributions. Controlled by STRAIN Case Control command.
|
| 3578
|
BAR STRAIN END A POINT F
|
Bar element strain at end A, strain recovery point F. For bar elements this strain will only include bending contributions. Controlled by STRAIN Case Control command.
|
| 3583
|
BAR STRAIN END B POINT C
|
Bar element strain at end B, strain recovery point C. For bar elements this strain will only include bending contributions. Controlled by STRAIN Case Control command.
|
| 3584
|
BAR STRAIN END B POINT D
|
Bar element strain at end B, strain recovery point D. For bar elements this strain will only include bending contributions. Controlled by STRAIN Case Control command.
|
| 3585
|
BAR STRAIN END B POINT E
|
Bar element strain at end B, strain recovery point E. For bar elements this strain will only include bending contributions. Controlled by STRAIN Case Control command.
|
| 3586
|
BAR STRAIN END B POINT F
|
Bar element strain at end B, strain recovery point F. For bar elements this strain will only include bending contributions. Controlled by STRAIN Case Control command.
|
| 3607
|
BAR STRAIN END A-AXIAL
|
Bar element axial strain at end A. Controlled by STRAIN Case Control command.
|
| 3608
|
BAR STRAIN END B-AXIAL
|
Bar element axial strain at end B. Controlled by STRAIN Case Control command.
|
| 3609
|
BAR STRAIN END A-MAX
|
Bar element maximum strain (bending and axial) for all points at end A. Controlled by STRAIN Case Control command.
|
| 3610
|
BAR STRAIN END A-MIN
|
Bar element minimum strain (bending and axial) for all points at end A. Controlled by STRAIN Case Control command.
|
| 3611
|
BAR STRAIN END B-MAX
|
Bar element maximum strain (bending and axial) for all points at end B. Controlled by STRAIN Case Control command.
|
| 3612
|
BAR STRAIN END B-MIN
|
Bar element minimum strain (bending and axial) for all points at end B. Controlled by STRAIN Case Control command.
|
| 3695
|
BAR VON MISES STRAIN
|
Bar element von Mises strain. Controlled by STRAIN Case Control command.
|
| 3940
|
BAR MAX STRAIN
|
Bar element maximum strain (bending and axial) for all points at ends A and B. Controlled by STRAIN Case Control command.
|
| 3941
|
BAR MIN STRAIN
|
Bar element minimum strain (bending and axial) for all points at ends A and B. Controlled by STRAIN Case Control command.
|
| 3998
|
BAR DAMAGE
|
Bar element fatigue damage. Controlled by
FATIGUE,
STRESS, and
STRAIN Case Control commands.
|
| 3999
|
BAR LIFE
|
Bar element fatigue life. Controlled by FATIGUE, STRESS, and STRAIN Case Control commands.
|