sr1992
Aerospace
- Sep 23, 2020
- 1
Hi everyone,
I am trying to do a multi step analysis of a 1d beam.
In step-1, I add point load to the cantilever.
Step-2, thermal loading on the deformed cantilever, so as to induce buckling.
However, the results do not seem to follow this trend. The results from the 1st step dissipate as the Step-2 progresses. All the loads from step 1 are carrying over to step-2. In addition, in step-2, i have applied a fixed boundary constraint at the free end (force applied end in Step-1). Restart analysis is not an option for 1d beam elements in abaqus/standard.
I would be appreciative any help.
Thanks,
*Heading
** Job name: Job-237 Model name: Job-234
** Generated by: Abaqus/CAE 2019
*Preprint, echo=NO, model=NO, history=NO, contact=NO
**
** PARTS
**
*Part, name=Part-1
*Node
1, -1970., 0.
2, -1770., 0.
3, -1570., 0.
4, -1370., 0.
5, -1170., 0.
6, -970., 0.
7, -770., 0.
8, -570., 0.
9, -370., 0.
10, -170., 0.
11, 30., 0.
*Element, type=B21
1, 1, 2
2, 2, 3
3, 3, 4
4, 4, 5
5, 5, 6
6, 6, 7
7, 7, 8
8, 8, 9
9, 9, 10
10, 10, 11
*Nset, nset=Set-1, generate
1, 11, 1
*Elset, elset=Set-1, generate
1, 10, 1
*Nset, nset=Set-2, generate
1, 11, 1
*Elset, elset=Set-2, generate
1, 10, 1
** Section: Section-1 Profile: Profile-2
*Beam Section, elset=Set-1, material=Material-1, poisson = 0.3, temperature=GRADIENTS, section=CIRC
50.
0.,0.,-1.
*End Part
**
**
** ASSEMBLY
**
*Assembly, name=Assembly
**
*Instance, name=Part-1-1, part=Part-1
*End Instance
**
*Nset, nset=Set-1, instance=Part-1-1
1,
*Nset, nset=Set-2, instance=Part-1-1
11,
*End Assembly
**
** MATERIALS
**
*Material, name=Material-1
*Density
7.9e-09,
*Elastic
210000., 0.3
*Expansion
0.0005,
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1, nlgeom=YES
*Static
0.01, 1., 1e-05, 0.1
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Symmetry/Antisymmetry/Encastre
*Boundary
Set-1, ENCASTRE
**
** LOADS
**
** Name: Load-1 Type: Concentrated force
*Cload
Set-2, 2, -15000.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field, variable=PRESELECT
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-2
**
*Step, name=Step-2, nlgeom=YES
*Static
0.01, 1., 1e-05, 0.1
**
** BOUNDARY CONDITIONS
**
** Name: BC-2 Type: Displacement/Rotation
*Boundary
Set-2, 1, 1
Set-2, 2, 2
Set-2, 6, 6
**
** PREDEFINED FIELDS
**
** Name: Predefined Field-1 Type: Temperature
*Temperature
Part-1-1.Set-1, 500.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field
*Node Output
CF, NT, RF, U, UR, UT, V, VR
VT
*Element Output, directions=YES
LE, PE, PEEQ, PEMAG, S, TEMP
*Contact Output
CDISP, CSTRESS
**
** FIELD OUTPUT: F-Output-2
**
*Node Output
U, UR, UT, V, VR, VT
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*End Step
I am trying to do a multi step analysis of a 1d beam.
In step-1, I add point load to the cantilever.
Step-2, thermal loading on the deformed cantilever, so as to induce buckling.
However, the results do not seem to follow this trend. The results from the 1st step dissipate as the Step-2 progresses. All the loads from step 1 are carrying over to step-2. In addition, in step-2, i have applied a fixed boundary constraint at the free end (force applied end in Step-1). Restart analysis is not an option for 1d beam elements in abaqus/standard.
I would be appreciative any help.
Thanks,
*Heading
** Job name: Job-237 Model name: Job-234
** Generated by: Abaqus/CAE 2019
*Preprint, echo=NO, model=NO, history=NO, contact=NO
**
** PARTS
**
*Part, name=Part-1
*Node
1, -1970., 0.
2, -1770., 0.
3, -1570., 0.
4, -1370., 0.
5, -1170., 0.
6, -970., 0.
7, -770., 0.
8, -570., 0.
9, -370., 0.
10, -170., 0.
11, 30., 0.
*Element, type=B21
1, 1, 2
2, 2, 3
3, 3, 4
4, 4, 5
5, 5, 6
6, 6, 7
7, 7, 8
8, 8, 9
9, 9, 10
10, 10, 11
*Nset, nset=Set-1, generate
1, 11, 1
*Elset, elset=Set-1, generate
1, 10, 1
*Nset, nset=Set-2, generate
1, 11, 1
*Elset, elset=Set-2, generate
1, 10, 1
** Section: Section-1 Profile: Profile-2
*Beam Section, elset=Set-1, material=Material-1, poisson = 0.3, temperature=GRADIENTS, section=CIRC
50.
0.,0.,-1.
*End Part
**
**
** ASSEMBLY
**
*Assembly, name=Assembly
**
*Instance, name=Part-1-1, part=Part-1
*End Instance
**
*Nset, nset=Set-1, instance=Part-1-1
1,
*Nset, nset=Set-2, instance=Part-1-1
11,
*End Assembly
**
** MATERIALS
**
*Material, name=Material-1
*Density
7.9e-09,
*Elastic
210000., 0.3
*Expansion
0.0005,
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1, nlgeom=YES
*Static
0.01, 1., 1e-05, 0.1
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Symmetry/Antisymmetry/Encastre
*Boundary
Set-1, ENCASTRE
**
** LOADS
**
** Name: Load-1 Type: Concentrated force
*Cload
Set-2, 2, -15000.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field, variable=PRESELECT
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-2
**
*Step, name=Step-2, nlgeom=YES
*Static
0.01, 1., 1e-05, 0.1
**
** BOUNDARY CONDITIONS
**
** Name: BC-2 Type: Displacement/Rotation
*Boundary
Set-2, 1, 1
Set-2, 2, 2
Set-2, 6, 6
**
** PREDEFINED FIELDS
**
** Name: Predefined Field-1 Type: Temperature
*Temperature
Part-1-1.Set-1, 500.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field
*Node Output
CF, NT, RF, U, UR, UT, V, VR
VT
*Element Output, directions=YES
LE, PE, PEEQ, PEMAG, S, TEMP
*Contact Output
CDISP, CSTRESS
**
** FIELD OUTPUT: F-Output-2
**
*Node Output
U, UR, UT, V, VR, VT
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*End Step