nas120 ws13 submarine buckling
TRANSCRIPT
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WORKSHOP 14
BUCKLING OF A SUBMARINEPRESSURE HULL
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Copyright 2005 MSC.Software Corporation
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Workshop Objectives
Create groups based on property sets.
Run a linear buckling analysis.
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Problem Description
A submarine pressure hull is modeled by plate and barelements.
Check the pressure hull for buckling at an operating depth of1000 ft which is equivalent to an external pressure of 445 psi.
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Suggested Exercise Steps
1. Create a new database and name it submarine.db.2. Import the MSC.Nastran input file pressure_hull.bdf.
3. Create groups based on property sets.
4. Post only the center pressure shell section.
5. Apply boundary conditions.6. Post the entire pressure shell.
7. Apply an external pressure of 445 psi to the pressure shell.
8. Run a linear buckling analysis. Request the first 5 roots (buckled
modes).9. Read the xdb file into MSC.Patran.
10. Post all the groups.
11. Plot the buckled mode shapes and identify which part of the pressure
hull is buckling for each mode.
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Step 2. Import File
a
b
c
Import the Nastran File
a. File: Import.b. Set the object to model and
the source to MSC.Nastran
Input.
c. Select pressure_hull.bdf.
d. Click Apply.
e. Click OK to Summary InputFile
d
Step 3 Create Groups
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Step 3. Create Groups
Create a new group
a. Group: Create.
b. Select Property Set as
the method.
c. Select Multiple Groups.
d. Click Apply.
a
b
c
d
Step 4 Post Entire Pressure Shell
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Step 4. Post Entire Pressure Shell
Post two groups
a. Group: Post.
b. Shift click to select
pshell.1 and
pshell.2.
c. Click Apply.
d. Click OK to change
the Current Group.
a
d
b
c
Step 5 Apply Boundary Conditions
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Step 5. Apply Boundary Conditions
Create a boundary condition
a. Loads/BCs: Create /
Displacement / Nodal.
b. Enterxyzconstraint as the
New Set Name.
c. Click Input Data.
d. Enter for
Translations and Rotations.
e. Click OK.
d
e
b
c
a
Step 5 Apply Boundary Conditions
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Apply the boundary condition
a. Click Select
Application Region.
b. For the Geometry
Filter select FEM.
c. Select the node at the
tip of the shell as
shown.
d. Click Add.
e. Click OK.
f. Click Apply.
e
d
b
c
Step 5. Apply Boundary Conditions
af
Step 7 Apply Pressure Load
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Step 7. Apply Pressure Load
Create a pressure load
a. Loads/BCs: Create /
Pressure / Element
Uniform.
b. Enterpressure_load as
the New Set Name.
c. Set the Target Element
Type to 2D.
d. Click Input Data.
e. Enter 445 for the Bottom
Surface Pressure.
f. Click OK.
e
f
b
a
c
d
Step 7 Apply Pressure Load
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Apply the boundary condition
a. Click Select
Application Region.
b. For the Geometry
Filter select FEM.c. Select the entire shell.
d. Click Add.
e. Click OK.
f. Click Apply.
e
d
b
Step 7. Apply Pressure Load
c
a
f
Step 8. Run Linear Buckling Analysis
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Step 8. Run Linear Buckling Analysis
Analyze the model
a. Analysis: Analyze /
Entire Model / Full
Run.
b. Enter submarine
as the job name.
c. Click Solution
Type.
d. Choose Buckling.
e. Click Solution
Parameters.f. Verify that the Plate
Rz Stiffness Factor
is 100.0
g. Click Eigenvalue
Extraction.
h. For the Number ofDesired Roots,
enter 5.
i. Click OK.
j. Click OK.
k. Click OK.
l. Click Apply.
a
c
d
eg
h
i
j
k
l
f
b
Step 9. Read Results into MSC.Patran
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Step 9. Read Results into MSC.Patran
Attach the results file
a. Analysis: Access Results /
Attach XDB / Result
Entities.
b. Click Select Results File.
c. Choose the results file
submarine.xdb.
d. Click OK.
e. Click Apply.
a
b
c
e
d
Step 10. Post All Groups
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p p
Post the default groupa. Group:Post.
b. Select default_group.
c. Click Apply.
d. Click on the Reset Graphics
Icon.
a
b
c
d
Step 11. Plot Mode Shapes
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Create a quick plot
a. Results: Create / Quick
Plot.
b. Select a Mode.
c. Select Eigenvectors,
Translational as the
Deformation Result.
d. Click Apply.
e. Repeat for other modes.
a
d
c
b
Step 11. Plot Mode Shapes
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p p
Record Data in the following table:
Mode No: Buckling Load Factor: Region of Buckling:
1 _________________ ______________________________
2 _________________ ______________________________
3 _________________ ______________________________
4 _________________ ______________________________
5 _________________ ______________________________