WS15 Submarine Buckling
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Transcript of WS15 Submarine Buckling
WORKSHOP 15
BUCKLING OF A SUBMARINE PRESSURE HULL
NAS120, Workshop 15, January 2003 WS15-1
WS15-2NAS120, Workshop 15, January 2003
WS15-3NAS120, Workshop 15, January 2003
Problem DescriptionA submarine pressure hull is modeled by plate and bar elements. Check the pressure hull for buckling at an operating depth of 1000 ft which is equivalent to an external pressure of 445 psi.
WS15-4NAS120, Workshop 15, January 2003
Workshop ObjectivesCreate groups based on property sets.Run a linear buckling analysis.
WS15-5NAS120, Workshop 15, January 2003
Suggested Exercise Steps1. 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.
WS15-6NAS120, Workshop 15, January 2003
Step 1. Create New Database
a
b c
d
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e
a
Create a new database called submarine.db
a. File / New.b. Enter submarine as the file
name.c. Click OK.d. Choose Default Tolerance.e. Select MSC.Nastran as the
Analysis Code.f. Select Structural as the
Analysis Type.g. Click OK.
WS15-7NAS120, Workshop 15, January 2003
Step 2. Import File
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c
d
a
Import the Nastran Filea. File: Import.b. Set the object to model
and the source to MSC.Nastran Input.
c. Select pressure_hull.bdf.
d. Click Apply.
WS15-8NAS120, Workshop 15, January 2003
Step 3. Create Groups
bc
d
a
Create a new groupa. Group: Create. b. Select Property Set as
the method.c. Select Multiple Groups.d. Click Apply.
WS15-9NAS120, Workshop 15, January 2003
Step 4. Post Entire Pressure Shell
b
a
c
Post two groupsa. Group: Post. b. Shift click to select
pshell.1 and pshell.2.c. Click Apply.
WS15-10NAS120, Workshop 15, January 2003
Step 5. Apply Boundary Conditions
b
c
d
e
a
Create a boundary conditiona. Loads/BCs: Create /
Displacement / Nodal.b. Enter xyzconstraint as the
New Set Name.c. Click Input Data.d. Enter <0 0 0> for
Translations and Rotations.e. Click OK.
WS15-11NAS120, Workshop 15, January 2003
Step 5. Apply Boundary Conditions
Apply the boundary conditiona. 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.
ae
f
d
b
c
WS15-12NAS120, Workshop 15, January 2003
Step 7. Apply Pressure Load
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a
c
Create a pressure loada. Loads/BCs: Create /
Pressure / Element Uniform.
b. Enter pressure_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.
WS15-13NAS120, Workshop 15, January 2003
Step 7. Apply Pressure Load
Apply the boundary conditiona. 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.
ae
f
d
b
c
WS15-14NAS120, Workshop 15, January 2003
Step 8. Run Linear Buckling Analysis
Analyze the modela. Analysis: Analyze /
Entire Model / Full Run.
b. Click Solution Type.
c. Choose Buckling.d. Click Solution
Parameters.e. Enter 100 for the
Plate Rz Stiffness Factor.
f. Click Eigenvaule Extraction.
g. For the Number of Desired Roots, enter 5.
h. Click OK.i. Click OK.j. Click OK. k. Click Apply.
a
b
c
df
g
h
i
j
k
e
WS15-15NAS120, Workshop 15, January 2003
Step 9. Read Results into MSC.Patran
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Attach the results filea. 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.
WS15-16NAS120, Workshop 15, January 2003
Step 10. Post All Groups
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Post the default groupa. Group:Post.b. Select default_group.c. Click Apply.d. Click on the Reset Graphics
Icon.
WS15-17NAS120, Workshop 15, January 2003
Step 11. Plot Mode Shapes
Create a quick plota. 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
WS15-18NAS120, Workshop 15, January 2003
Step 11. Plot Mode Shapes
Record Data in the following table:
Mode: Factor: Region of Buckling:
1 ______ _____________________________________
2 ______ _____________________________________
3 ______ _____________________________________
4 ______ _____________________________________
5 ______ _____________________________________