ws14 rect plate modes

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    WORKSHOP 14

    NORMAL MODES OF ARECTANGULAR PLATE

    NAS120, Workshop 14, January 2003 WS14-1

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    WS14-2NAS120, Workshop 14, January 2003

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    WS14-3NAS120, Workshop 14, January 2003

    Problem Description

    A rectangular plate is simply supported at all edges. Find the first 10normal modes for this plate.

    E = 10 x 106 psi

    =0.33

    = 0.101 lb/in3

    t = 0.125 in

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    Workshop Objectives

    Perform a normal modes analysis on a rectangular plate.

    Evaluate the quality of the normal modes solution graphically.

    Compare analysis results to theoretical results.

    Evaluate the effect of varying mesh density.

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    Suggested Exercise Steps

    1. Create a new database and name it rectangular_plate1.db.

    2. Create a rectangular surface.

    3. Mesh the surface to create plate elements.

    4. Create material properties. Dont forget to enter density.

    5. Create physical properties.

    6. Apply Loads and Boundary Conditions.

    7. Perform a normal modes analysis to determine the first 10 modes for the plate.

    8. Read the results into MSC.Patran.

    9. Plot the mode shapes. Visually evaluate the quality of the mode shapes.

    10. Compare the first natural frequency to theoretical results.

    11. File / save a copy as rectangular_plate2.db.

    12. Close the database and open the rectangular_plate2 database.

    13. Delete the original results file.

    14. Re-mesh the surface. Use a global edge length of 0.5 in.

    15. Re-run the analysis.

    16. Attach the new results file to the database.

    17. Plot the mode shapes.

    18. Compare the results from the finer mesh with the earlier results.

    St 1 C t N D t b

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    Step 1. Create New Database

    a

    b c

    d

    f

    g

    e

    a

    Create a new database called

    rectangular_plate1.db

    a. File / New.b. Enter rectangular_plate1 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.

    St 2 C t R t l S f

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    Step 2. Create a Rectangular Surface

    Create a surface

    a. Geometry: Create /

    Surface / XYZ.

    b. Enter for theVector Coordinates list.

    c. Click Apply.

    b

    c

    a

    Step 3 Mesh the Surface

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    Step 3. Mesh the Surface

    Create a surface mesh

    a. Elements: Create / Mesh

    / Surface.

    b. Select the surface.

    c. Enter 1.4 for the Global

    Edge Length.

    d. Click Apply.

    a

    b

    c

    d

    Step 4 Create Material Properties

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    Step 4. Create Material Properties

    a

    c

    b

    d

    hg

    e

    f

    Create an isotropic material

    a. Materials: Create / Isotropic

    / Manual Input.

    b. Enter plate_material for

    the Material Name.

    c. Click Input Properties.

    d. Enter 10e6 for the Elastic

    Modulus.

    e. Enter 0.33 for the Poisson

    Ratio.

    f. Enter 0.101 for the Density.

    g. Click OK.

    h. Click Apply.

    Step 5 Create Physical Properties

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    Step 5. Create Physical Properties

    a

    b

    c

    f

    d

    e

    Create physical properties

    a. Properties: Create / 2D /

    Shell.

    b. Enter plate_prop as theProperty Set Name.

    c. Click Input Properties.

    d. Select plate_material as

    the material.

    e. Enter 0.125 for the

    Thickness.f. Click OK.

    Step 5 Create Physical Properties

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    Step 5. Create Physical Properties

    a

    b

    c

    d

    e

    Apply the physical properties

    a. Properties: Create / 2D

    / Shell.

    b. Click in the SelectMembers box.

    c. Rectangular pick the

    entire plate as shown.

    d. Click Add.

    e. Click Apply.

    Step 6 Apply Loads and Boundary Conditions

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    Step 6. Apply Loads and Boundary Conditions

    b

    c

    d

    e

    a

    Create a boundary condition

    a. Loads/BCs: Create /

    Displacement / Nodal.

    b. Enter simple_support as

    the New Set Name.

    c. Click Input Data.

    d. Enter for

    Translations

    e. Click OK.

    Step 6 Apply Loads and Boundary Conditions

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    WS14-13NAS120, Workshop 14, January 2003

    Step 6. Apply Loads and Boundary Conditions

    Apply the boundary condition

    a. Click Select

    Application Region.

    b. For the Geometry

    Filter selectGeometry.

    c. Set the Selection

    Filter to Curve or

    Edge and select an

    edge.

    d. Click Add.e. Repeat the procedure

    until all four edges

    have been added.

    f. Click OK.

    g. Click Apply.

    af

    g

    d

    b

    c

    Step 7. Run Normal Modes Analysis

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    WS14-14NAS120, Workshop 14, January 2003

    Step 7. Run Normal Modes Analysis

    Analyze the model

    a. Analysis: Analyze / Entire

    Model / Full Run.

    b. Click Solution Type.

    c. Choose Normal Modes.

    d. Click Solution Parameters.

    e. Enter 0.00259 for Wt.-Mass

    conversion.

    f. Click OK.

    g. Click OK.h. Click Apply.

    f

    e

    a

    h

    b

    c

    g

    d

    Step 8. Read Results into MSC.Patran

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    WS14-15NAS120, Workshop 14, January 2003

    Step 8. Read Results into MSC.Patran

    a

    b

    c

    e

    d

    Attach the results file

    a. Analysis: Access Results /

    Attach XDB / Result

    Entities.

    b. Click Select Results File.

    c. Choose the results file

    Rectangular_plate1.xdb.

    d. Click OK.

    e. Click Apply.

    Step 9. Plot Mode Shapes

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    WS14-16NAS120, Workshop 14, January 2003

    p p

    a

    c

    b

    Create a quick plot

    a. Results: Create / Quick

    Plot.

    b. Select Eigenvectors,

    Translational as theDeformation Result.

    c. Click Apply.

    First 10 modes:

    1_________ 6_________

    2_________ 7_________

    3_________ 8_________

    4_________ 9_________

    5_________ 10________

    Step 10. Compare to Theoretical Results

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    WS14-17NAS120, Workshop 14, January 2003

    p p

    Theoretical results based on Formulas for Natural Frequency

    and Mode Shape, 1984 edition, Table 11-4, case 16

    )(2

    =

    112

    tE

    a2

    f

    3

    2

    21

    1

    a = 12, b = 8, a/b = 1.5

    12 = 32.08

    E = 10 x 106

    t = 0.125

    = 0.33

    = 0.101/386.1 = 2.616 x 10-4

    = . t = 3.270 x 10-5

    f1 = 265 Hz

    Step 11. Save a Copy

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    WS14-18NAS120, Workshop 14, January 2003

    p py

    a

    b c

    Save a copy of the file

    a. File: Save a Copy.b. Type rectangular_plate2

    as the file name.

    c. Click Save.

    Step 12. Open the New Database

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    WS14-19NAS120, Workshop 14, January 2003

    a

    b

    c

    d

    Close the original file and open

    the new file

    a. File: Close.

    b. File: Open.

    c. Select the file:

    rectangular_plate2.db .

    d. Click OK.

    Step 13. Delete Old Results File

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    WS14-20NAS120, Workshop 14, January 2003

    e

    Delete XDB attachment

    a. Analysis: Delete / XDB

    Attachment.

    b. Select the

    rectangular_plate1.xdb attachment.

    c. Click Apply.

    d. ChooseYes to delete

    the attachment.

    e. Click on the front view

    icon.

    d

    a

    b

    c

    Step 14. Re-Mesh the Surface

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    WS14-21NAS120, Workshop 14, January 2003

    a

    b

    c

    d

    e

    Create a finer mesh

    a. Elements: Create / Mesh

    / Surface.

    b. Select the entire surface.

    c. Enter 0.5 for the Global

    Edge Length.

    d. Click Apply.

    e. ChooseYes to delete

    the existing mesh.

    Step 15. Run Normal Modes Analysis

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    WS14-22NAS120, Workshop 14, January 2003

    Analyze the model

    a. Analysis: Analyze /

    Entire Model / Full

    Run.

    b. Change the jobname to:

    rectangular_plate2.

    c. Click Apply.

    a

    b

    c

    Step 16. Attach New Results File

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    WS14-23NAS120, Workshop 14, January 2003

    a

    b

    e

    Attach the results file

    a. Analysis: Access Results /

    Attach XDB / Result

    Entities.

    b. Click Select Results File.c. Choose the results file

    rectangular_plate2 .xdb.

    d. Click OK.

    e. Click Apply.

    c

    d

    Step 17. Plot Mode Shapes

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    WS14-24NAS120, Workshop 14, January 2003

    Create a quick plot

    a. Results: Create / Quick

    Plot.

    b. Select Eigenvectors,

    Translational as theDeformation Result.

    c. Click Apply.

    First 10 modes:

    1_________ 6_________

    2_________ 7_________

    3_________ 8_________

    4_________ 9_________

    5_________ 10________

    a

    c

    b