SlideShare a Scribd company logo
Workshop 7
Step Definition and Loads: Pipe Creep Model
Defining steps and specifying output requests
You will now define the analysis steps. For this simulation you will define two static,
general steps. In the first step a pressure load is applied; in the second step a transient
analysis is carried out to determine the creep of the pressurized vessel.
In addition, you will specify output requests for your analysis. Moreover, since
interactions, loads, and boundary conditions can be step dependent, analysis steps must be
defined before these can be specified.
To begin this workshop, start a new session of ABAQUS/CAE from the
workshops/pipeCreep directory. Open the database containing the pipe creep
model.
To define a step:
1. From the Module list located under the toolbar, select Step to enter the Step
module.
2. From the main menu bar, select StepCreate to create an analysis step. In the
Create Step dialog box that appears, name the step Pressure and accept the
General procedure type. From the list of available procedure options, accept
Static, General. Click Continue.
3. In the Edit Step dialog box that appears, enter the following step description:
Apply internal pressure. Accept the default settings, and click OK.
4. From the main menu bar, select StepCreate to create another analysis step.
Insert the new step after the one created earlier. In the Create Step dialog box
that appears, name the step Creep and accept the General procedure type. From
the list of available procedure options, select Visco. Click Continue.
5. In the Edit Step dialog box that appears, enter the following step description:
Transient creep. Set the time period for the step to 4.38E5 hours
(approximately 50 years). Use initial and minimum time increments of 1.0 hour
and a maximum time increment of 4.38E5 hours. Set the tolerance for the
maximum difference in the creep strain increment (CETOL) to 1.0E5 and the
maximum number of increments to 1000.
Since you will use ABAQUS/Viewer to postprocess the results, you must specify the
output data you wish to have written to the output database (.odb) file. Default
history and field output requests are selected automatically by ABAQUS/CAE for
each procedure type. This output is sufficient for the first step (Pressure). For the
second step (Creep), however, we require only the following output:
· The displacements, stresses, and creep strains (written as field data to the output
database file every 2 increments).
· The displacements for the point shown in Figure W7–1 (written as history data every
two increments).
Figure W7–1. Region for restricted output
The history output request requires a set to be defined. Follow the steps outlined
below to define a set and request output.
To define a set:
1. From the main menu bar, select ToolsSetCreate. In the Create Set dialog
box, name the set Out and click Continue.
6. Select the point indicated in Figure W7–1.
7. Click Done in the prompt area when the appropriate region is highlighted in the
viewport.
To specify output requests to the output database file:
1. From the main menu bar, select OutputField Output Requests
Manager. In the Field Output Requests Manager, select the cell labeled
Propagated in the column labeled Creep. The information at the bottom of the
dialog box indicates that preselected default field output requests have been made
for this step.
W7.2
set Out
8. On the right side of the dialog box, click Edit to change the field output requests.
In the Edit Field Output Request dialog box that appears:
A. Click the arrow next to Stresses to show the list of available stress output.
Accept the default selection of stress components and invariants.
B. Click the arrow next to Strains to show the list of available strain output.
Toggle off PE, PEEQ, and PEMAG.
C. Toggle off Forces/Reactions and Contact.
D. Accept the default Displacement/Velocity/Acceleration output.
E. Save the output every 2 increments.
F. Click OK.
G. Click Dismiss to close the Field Output Requests Manager.
9. Modify the history output by selecting OutputHistory Output
RequestsManager. In the History Output Requests Manager, select
the cell labeled Created in the column labeled Pressure if it is not already
selected. On the right side of the dialog box, click Edit.
A. Toggle on Set name as the domain and, from the list of available sets,
choose Out.
H. Toggle off Energy in the Output Variables region.
I. Select the displacement components (U under Displacement/Velocity/
Acceleration).
J. Save the output every 2 increments.
K. Click OK.
L. Click Dismiss to close the History Output Requests Manager.
Prescribing boundary conditions and applied loads
Symmetry conditions must be applied to the two symmetry planes in the model. In
addition, a single point must be restrained in the vertical direction to prevent rigid body
motion.
Both the pipe and the pressure vessel are assumed to be operating under an internal
pressure of 1.4E7 Pa. In addition, the pipe and pressure vessel are subject to end cap load
conditions. This implies that for any cut through the model, the equivalent load due to the
pressure on the cap can be applied as traction loads on the cut section. Hand calculations
provide that the equivalent traction loads are: 8.281E6 Pa for the pressure vessel and
7.682E6 Pa for the pipe. Furthermore, depending on the proximity of the cuts to the
critical stress region, the boundary conditions could include multipoint constraints that
would require that plane cut sections remain plane. For this exercise we will assume that
the cuts are made a sufficient distance from the area of interest, and this last requirement
will be ignored.
The pipe is at a uniform initial temperature of 540º
C.
To prescribe boundary conditions:
1. From the Module list located under the toolbar, select Load to enter the Load
module.
W7.3
10. From the main menu bar, select BCCreate to prescribe boundary conditions
on the model. In the Create Boundary Condition dialog box that appears,
name the boundary condition X-SYMM and select Initial as the step in which it
will be applied. Accept Mechanical as the category and Symmetry/
Antisymmetry/Encastre as the type. Click Continue.
You may need to rotate the view to facilitate your selection in the following steps.
11. Select ViewRotate from the main menu bar (or use the tool from the
toolbar), and drag the cursor over the virtual trackball in the viewport. The view
rotates interactively; try dragging the cursor inside and outside the virtual
trackball to see the difference in behavior.
12. Select the regions of the model indicated in Figure W7–2 using [Shift]+Click.
Click Done in the prompt area when the appropriate regions are highlighted in
the viewport, and toggle on XSYMM in the Edit Boundary Condition dialog
box that appears. Click OK to apply the boundary condition.
Figure W7–2. XSYMM boundary condition region
Arrows appear on the face indicating the constrained degrees of freedom. The
XSYMM boundary condition constrains the degrees of freedom necessary to
impose symmetry about a plane X = constant; after the part is meshed and the job
is created, this constraint will be applied to all the nodes that occupy the region.
W7.4
XSYMM regions
13. Repeat steps 2 through 4 to apply a ZSYMM boundary condition to the region
shown in Figure W7–3. Name the boundary condition Z-SYMM.
Figure W7–3. ZSYMM boundary condition region
To satisfy the end cap condition on the intersecting pipe, apply a displacement constraint
normal to the entire face of the free end of the pipe. This action will constrain the model
against rigid body motion, and the equivalent traction loads will be generated as reaction
forces.
14. From the main menu bar, select BCCreate. In the Create Boundary
Condition dialog box that appears, name the boundary condition EndCap, and
select Initial as the step in which it will be applied. Accept Mechanical as the
category and select Displacement/Rotation as the type. Click Continue.
15. Select the region of the model indicated in Figure W7–4 using the cursor. Click
Done in the prompt area when the appropriate region is highlighted in the
viewport, and toggle on U2 in the Edit Boundary Condition dialog box that
appears. Click OK to apply the boundary condition.
W7.5
ZSYMM region
Figure W7–4. U2 boundary condition region
To apply a pressure load:
1. From the main menu bar, select LoadCreate to prescribe the internal pressure
load. In the Create Load dialog box that appears, name the load Internal
Pressure and select Pressure as the step in which it will be applied. Accept
Mechanical as the category, and select Pressure as the type. Click Continue.
16. Select the surfaces associated with the interior of the pipe and pressure vessel
using the cursor; the region is highlighted in Figure W7–5. When the appropriate
surfaces are selected, click Done in the prompt area.
W7.6
Fix U2 at top of pipe
Figure W7–5. Surface to which internal pressure will be applied
17. Specify a uniform pressure of 1.4E7 in the Edit Load dialog box, and click OK
to apply the load.
Arrows appear on the model faces indicating the applied load.
Next, apply a pressure load to impose the end cap condition on the pressure
vessel.
18. Repeat steps 1 through 3 above to apply a pressure of 8.281E6 Pa to the region
highlighted in Figure W7–6. Name the load Vessel End Cap.
W7.7
inner surface
Figure W7–6. Surface to which end cap pressure will be applied
To apply an initial temperature:
1. From the main menu bar, select FieldCreate to prescribe the initial
temperature. In the Create Field dialog box that appears, name the field
InitialTemp and select Initial as the step in which it will be applied. Select
Other as the category and Temperature as the type. Click Continue.
19. Select the entire model as the region to which the field will be applied.
20. Click Done in the prompt area when the appropriate region is highlighted in the
viewport.
21. Specify a uniform temperature of 540º
C in the Edit Field dialog box, and click
OK to apply the field.
22. Save your model database, and exit your ABAQUS/CAE session.
W7.8
Apply end cap pressure to
this surface

More Related Content

PDF
Workshop9 pump-mesh2005
PDF
Workshop12 skewplate
PDF
Workshop5 pump-mat
PDF
Workshop14 pipe-whip
PDF
Workshop2 creep-geo
PDF
Workshop10 creep-jop
PDF
Workshop16 heat-pipejoint
PDF
Workshop4 creep-props
Workshop9 pump-mesh2005
Workshop12 skewplate
Workshop5 pump-mat
Workshop14 pipe-whip
Workshop2 creep-geo
Workshop10 creep-jop
Workshop16 heat-pipejoint
Workshop4 creep-props

What's hot (20)

PDF
Workshop3 pump-geo
PDF
Workshop1 cant-beam
PDF
Workshop11 beam-load-cases
PDF
Workshop8 creep-mesh
PDF
Workshop13 pump-analysis
PDF
Workshop15 rolling-plate
PDF
Workshop6 pump-assy
PDF
Workshop9 pump-mesh
PDF
Safe tutorial
PDF
Tutorial for design of foundations using safe
PDF
02 release document_8.8
PDF
How to model and analyse structures using etabs
PDF
Rcc structure design by etabs (acecoms)
PDF
Etabs tutorial
PDF
4. safe tutorial v. 12 ingles
PDF
Creo 3.0 tips and tricks r4
PDF
App4 time history analysis
PDF
Tower design using etabs- Nada Zarrak
PDF
Creo parametric tips and tricks
PDF
Etabs mate quick start en
Workshop3 pump-geo
Workshop1 cant-beam
Workshop11 beam-load-cases
Workshop8 creep-mesh
Workshop13 pump-analysis
Workshop15 rolling-plate
Workshop6 pump-assy
Workshop9 pump-mesh
Safe tutorial
Tutorial for design of foundations using safe
02 release document_8.8
How to model and analyse structures using etabs
Rcc structure design by etabs (acecoms)
Etabs tutorial
4. safe tutorial v. 12 ingles
Creo 3.0 tips and tricks r4
App4 time history analysis
Tower design using etabs- Nada Zarrak
Creo parametric tips and tricks
Etabs mate quick start en
Ad

Similar to Workshop7 creep-steps (20)

PPTX
Modelling for etab and design on etabs for concrete
PPTX
etab modelling and design of concrete elemnts
PPT
Naka_airfoil_0012_simulation_ansys_cfx_1.ppt
PDF
Ansys iges tutorial
PPTX
PowerWorld 15. Transient Stability Quickstart
PDF
WORKSHOP STIFFENED PLATE WITH SOFTWARE PATRAN
PDF
Structural Analysis and Optimization of Buckling Strength through Stiffeners ...
PDF
Tutorial ic design
PDF
Modeling seismic analysis_and_design_of_rc_building_10_story
PDF
Sap tutorial for dynamics
PPT
[Point] pipe stress analysis by computer-caesar ii
PPT
Pipe Stress Analysis by Computer-CAESAR II.ppt
PDF
Manual check using staadpro
PDF
Appliedfluidmechanics6emot 121205015001-phpapp01
PDF
Cadence manual
PDF
Eppendorf mastercyclertechnote
PDF
CAD Lab Manual 2021-22 pdf-30-51.pdf
PDF
Normal Modal Analysis in Hypermesh
PDF
Fracture Toughness Testing for materials
Modelling for etab and design on etabs for concrete
etab modelling and design of concrete elemnts
Naka_airfoil_0012_simulation_ansys_cfx_1.ppt
Ansys iges tutorial
PowerWorld 15. Transient Stability Quickstart
WORKSHOP STIFFENED PLATE WITH SOFTWARE PATRAN
Structural Analysis and Optimization of Buckling Strength through Stiffeners ...
Tutorial ic design
Modeling seismic analysis_and_design_of_rc_building_10_story
Sap tutorial for dynamics
[Point] pipe stress analysis by computer-caesar ii
Pipe Stress Analysis by Computer-CAESAR II.ppt
Manual check using staadpro
Appliedfluidmechanics6emot 121205015001-phpapp01
Cadence manual
Eppendorf mastercyclertechnote
CAD Lab Manual 2021-22 pdf-30-51.pdf
Normal Modal Analysis in Hypermesh
Fracture Toughness Testing for materials
Ad

Recently uploaded (20)

PDF
01-Introduction-to-Information-Management.pdf
PDF
ChatGPT for Dummies - Pam Baker Ccesa007.pdf
PDF
Anesthesia in Laparoscopic Surgery in India
PDF
RTP_AR_KS1_Tutor's Guide_English [FOR REPRODUCTION].pdf
PDF
Chapter 2 Heredity, Prenatal Development, and Birth.pdf
PDF
Chinmaya Tiranga quiz Grand Finale.pdf
PDF
GENETICS IN BIOLOGY IN SECONDARY LEVEL FORM 3
PPTX
1st Inaugural Professorial Lecture held on 19th February 2020 (Governance and...
PDF
OBE - B.A.(HON'S) IN INTERIOR ARCHITECTURE -Ar.MOHIUDDIN.pdf
PDF
Updated Idioms and Phrasal Verbs in English subject
PDF
2.FourierTransform-ShortQuestionswithAnswers.pdf
PPTX
Radiologic_Anatomy_of_the_Brachial_plexus [final].pptx
PDF
grade 11-chemistry_fetena_net_5883.pdf teacher guide for all student
PPTX
Microbial diseases, their pathogenesis and prophylaxis
PDF
Computing-Curriculum for Schools in Ghana
PDF
A systematic review of self-coping strategies used by university students to ...
PDF
Practical Manual AGRO-233 Principles and Practices of Natural Farming
PDF
A GUIDE TO GENETICS FOR UNDERGRADUATE MEDICAL STUDENTS
PPTX
master seminar digital applications in india
PPTX
Tissue processing ( HISTOPATHOLOGICAL TECHNIQUE
01-Introduction-to-Information-Management.pdf
ChatGPT for Dummies - Pam Baker Ccesa007.pdf
Anesthesia in Laparoscopic Surgery in India
RTP_AR_KS1_Tutor's Guide_English [FOR REPRODUCTION].pdf
Chapter 2 Heredity, Prenatal Development, and Birth.pdf
Chinmaya Tiranga quiz Grand Finale.pdf
GENETICS IN BIOLOGY IN SECONDARY LEVEL FORM 3
1st Inaugural Professorial Lecture held on 19th February 2020 (Governance and...
OBE - B.A.(HON'S) IN INTERIOR ARCHITECTURE -Ar.MOHIUDDIN.pdf
Updated Idioms and Phrasal Verbs in English subject
2.FourierTransform-ShortQuestionswithAnswers.pdf
Radiologic_Anatomy_of_the_Brachial_plexus [final].pptx
grade 11-chemistry_fetena_net_5883.pdf teacher guide for all student
Microbial diseases, their pathogenesis and prophylaxis
Computing-Curriculum for Schools in Ghana
A systematic review of self-coping strategies used by university students to ...
Practical Manual AGRO-233 Principles and Practices of Natural Farming
A GUIDE TO GENETICS FOR UNDERGRADUATE MEDICAL STUDENTS
master seminar digital applications in india
Tissue processing ( HISTOPATHOLOGICAL TECHNIQUE

Workshop7 creep-steps

  • 1. Workshop 7 Step Definition and Loads: Pipe Creep Model Defining steps and specifying output requests You will now define the analysis steps. For this simulation you will define two static, general steps. In the first step a pressure load is applied; in the second step a transient analysis is carried out to determine the creep of the pressurized vessel. In addition, you will specify output requests for your analysis. Moreover, since interactions, loads, and boundary conditions can be step dependent, analysis steps must be defined before these can be specified. To begin this workshop, start a new session of ABAQUS/CAE from the workshops/pipeCreep directory. Open the database containing the pipe creep model. To define a step: 1. From the Module list located under the toolbar, select Step to enter the Step module. 2. From the main menu bar, select StepCreate to create an analysis step. In the Create Step dialog box that appears, name the step Pressure and accept the General procedure type. From the list of available procedure options, accept Static, General. Click Continue. 3. In the Edit Step dialog box that appears, enter the following step description: Apply internal pressure. Accept the default settings, and click OK. 4. From the main menu bar, select StepCreate to create another analysis step. Insert the new step after the one created earlier. In the Create Step dialog box that appears, name the step Creep and accept the General procedure type. From the list of available procedure options, select Visco. Click Continue. 5. In the Edit Step dialog box that appears, enter the following step description: Transient creep. Set the time period for the step to 4.38E5 hours (approximately 50 years). Use initial and minimum time increments of 1.0 hour and a maximum time increment of 4.38E5 hours. Set the tolerance for the maximum difference in the creep strain increment (CETOL) to 1.0E5 and the maximum number of increments to 1000. Since you will use ABAQUS/Viewer to postprocess the results, you must specify the output data you wish to have written to the output database (.odb) file. Default history and field output requests are selected automatically by ABAQUS/CAE for each procedure type. This output is sufficient for the first step (Pressure). For the second step (Creep), however, we require only the following output: · The displacements, stresses, and creep strains (written as field data to the output database file every 2 increments).
  • 2. · The displacements for the point shown in Figure W7–1 (written as history data every two increments). Figure W7–1. Region for restricted output The history output request requires a set to be defined. Follow the steps outlined below to define a set and request output. To define a set: 1. From the main menu bar, select ToolsSetCreate. In the Create Set dialog box, name the set Out and click Continue. 6. Select the point indicated in Figure W7–1. 7. Click Done in the prompt area when the appropriate region is highlighted in the viewport. To specify output requests to the output database file: 1. From the main menu bar, select OutputField Output Requests Manager. In the Field Output Requests Manager, select the cell labeled Propagated in the column labeled Creep. The information at the bottom of the dialog box indicates that preselected default field output requests have been made for this step. W7.2 set Out
  • 3. 8. On the right side of the dialog box, click Edit to change the field output requests. In the Edit Field Output Request dialog box that appears: A. Click the arrow next to Stresses to show the list of available stress output. Accept the default selection of stress components and invariants. B. Click the arrow next to Strains to show the list of available strain output. Toggle off PE, PEEQ, and PEMAG. C. Toggle off Forces/Reactions and Contact. D. Accept the default Displacement/Velocity/Acceleration output. E. Save the output every 2 increments. F. Click OK. G. Click Dismiss to close the Field Output Requests Manager. 9. Modify the history output by selecting OutputHistory Output RequestsManager. In the History Output Requests Manager, select the cell labeled Created in the column labeled Pressure if it is not already selected. On the right side of the dialog box, click Edit. A. Toggle on Set name as the domain and, from the list of available sets, choose Out. H. Toggle off Energy in the Output Variables region. I. Select the displacement components (U under Displacement/Velocity/ Acceleration). J. Save the output every 2 increments. K. Click OK. L. Click Dismiss to close the History Output Requests Manager. Prescribing boundary conditions and applied loads Symmetry conditions must be applied to the two symmetry planes in the model. In addition, a single point must be restrained in the vertical direction to prevent rigid body motion. Both the pipe and the pressure vessel are assumed to be operating under an internal pressure of 1.4E7 Pa. In addition, the pipe and pressure vessel are subject to end cap load conditions. This implies that for any cut through the model, the equivalent load due to the pressure on the cap can be applied as traction loads on the cut section. Hand calculations provide that the equivalent traction loads are: 8.281E6 Pa for the pressure vessel and 7.682E6 Pa for the pipe. Furthermore, depending on the proximity of the cuts to the critical stress region, the boundary conditions could include multipoint constraints that would require that plane cut sections remain plane. For this exercise we will assume that the cuts are made a sufficient distance from the area of interest, and this last requirement will be ignored. The pipe is at a uniform initial temperature of 540º C. To prescribe boundary conditions: 1. From the Module list located under the toolbar, select Load to enter the Load module. W7.3
  • 4. 10. From the main menu bar, select BCCreate to prescribe boundary conditions on the model. In the Create Boundary Condition dialog box that appears, name the boundary condition X-SYMM and select Initial as the step in which it will be applied. Accept Mechanical as the category and Symmetry/ Antisymmetry/Encastre as the type. Click Continue. You may need to rotate the view to facilitate your selection in the following steps. 11. Select ViewRotate from the main menu bar (or use the tool from the toolbar), and drag the cursor over the virtual trackball in the viewport. The view rotates interactively; try dragging the cursor inside and outside the virtual trackball to see the difference in behavior. 12. Select the regions of the model indicated in Figure W7–2 using [Shift]+Click. Click Done in the prompt area when the appropriate regions are highlighted in the viewport, and toggle on XSYMM in the Edit Boundary Condition dialog box that appears. Click OK to apply the boundary condition. Figure W7–2. XSYMM boundary condition region Arrows appear on the face indicating the constrained degrees of freedom. The XSYMM boundary condition constrains the degrees of freedom necessary to impose symmetry about a plane X = constant; after the part is meshed and the job is created, this constraint will be applied to all the nodes that occupy the region. W7.4 XSYMM regions
  • 5. 13. Repeat steps 2 through 4 to apply a ZSYMM boundary condition to the region shown in Figure W7–3. Name the boundary condition Z-SYMM. Figure W7–3. ZSYMM boundary condition region To satisfy the end cap condition on the intersecting pipe, apply a displacement constraint normal to the entire face of the free end of the pipe. This action will constrain the model against rigid body motion, and the equivalent traction loads will be generated as reaction forces. 14. From the main menu bar, select BCCreate. In the Create Boundary Condition dialog box that appears, name the boundary condition EndCap, and select Initial as the step in which it will be applied. Accept Mechanical as the category and select Displacement/Rotation as the type. Click Continue. 15. Select the region of the model indicated in Figure W7–4 using the cursor. Click Done in the prompt area when the appropriate region is highlighted in the viewport, and toggle on U2 in the Edit Boundary Condition dialog box that appears. Click OK to apply the boundary condition. W7.5 ZSYMM region
  • 6. Figure W7–4. U2 boundary condition region To apply a pressure load: 1. From the main menu bar, select LoadCreate to prescribe the internal pressure load. In the Create Load dialog box that appears, name the load Internal Pressure and select Pressure as the step in which it will be applied. Accept Mechanical as the category, and select Pressure as the type. Click Continue. 16. Select the surfaces associated with the interior of the pipe and pressure vessel using the cursor; the region is highlighted in Figure W7–5. When the appropriate surfaces are selected, click Done in the prompt area. W7.6 Fix U2 at top of pipe
  • 7. Figure W7–5. Surface to which internal pressure will be applied 17. Specify a uniform pressure of 1.4E7 in the Edit Load dialog box, and click OK to apply the load. Arrows appear on the model faces indicating the applied load. Next, apply a pressure load to impose the end cap condition on the pressure vessel. 18. Repeat steps 1 through 3 above to apply a pressure of 8.281E6 Pa to the region highlighted in Figure W7–6. Name the load Vessel End Cap. W7.7 inner surface
  • 8. Figure W7–6. Surface to which end cap pressure will be applied To apply an initial temperature: 1. From the main menu bar, select FieldCreate to prescribe the initial temperature. In the Create Field dialog box that appears, name the field InitialTemp and select Initial as the step in which it will be applied. Select Other as the category and Temperature as the type. Click Continue. 19. Select the entire model as the region to which the field will be applied. 20. Click Done in the prompt area when the appropriate region is highlighted in the viewport. 21. Specify a uniform temperature of 540º C in the Edit Field dialog box, and click OK to apply the field. 22. Save your model database, and exit your ABAQUS/CAE session. W7.8 Apply end cap pressure to this surface