Ws03_directtransient

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    WS3-1

    WORKSHOP 3

    DIRECT TRANSIENT ANALYSIS

    NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

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    WS3-2NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

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    WS3-3NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    DIRECT TRANSIENT RESPONSE

    Problem Description Using the direct method, determine the transient response of the

    flat rectangular plate, created in Workshop 1a, subject to time-

    varying excitation. This example structure is excited by 1 psi

    pressure load over the total surface of the plate varying at 250 Hz.

    In addition, a 50 lb force is applied at a corner of the tip also

    varying for the duration of 0.008 seconds only. Use structuraldamping of g = 0.06 and convert this damping to equivalent viscous

    damping at 250 Hz. Carry the analysis for 0.04 seconds.

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    WS3-4NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    DIRECT TRANSIENT RESPONSE

    Problem Description (cont.) Below is a finite element representation of the flat plate. It also

    contains the loads and boundary constraints.

    1 p s i o ve r t h e t o ta l su r f a ce

    50.00

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    WS3-5NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    DIRECT TRANSIENT RESPONSE

    Suggested Exercise Steps1. Import the model from Workshop 1a.

    2. Create a non-spatial field for the pressure load and the force load.

    3. Create a time dependent load case.

    4. Create the time dependent force load.

    5. Create the time dependent pressure load.

    6. Submit the model to MSC.Nastran for analysis.7. Attach the .XDB results file.

    8. Post Process results create X vs Y graph of displacements.

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    WS3-6NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    CREATE NEW DATABASE

    Create a new database calledws3.db.

    a. File / New.

    b. Enterws3 as the file name.

    c. Click OK.

    d. Choose Default Tolerance.

    e. Select MSC.Nastran as theAnalysis Code.

    f. Select Structural as theAnalysis Type.

    g. Click OK.

    a

    bc

    d

    e

    f

    g

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    WS3-7NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 1. File / Import

    Import the model from Workshop 1a.

    a. File / Import.

    b. Select MSC.Patran DB as theSource.

    c. Select ws1a.db.

    d. Click Apply.

    e. Click OK when the PatranDatabase Import Summaryappears.

    a

    bc

    d

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    WS3-8NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 2. Field: Create / Non Spatial / Tabular Input

    Create a Non Spatial field forthe pressure load.

    a. Fields: Create / NonSpatial / TabularInput.

    b. Enterpressure forthe Field Name.

    c. Select Time (t) as theActive IndependentVariable.

    d. Click Input Data.

    e. Click Map Functionto Table.

    f. Type in the function,sind(250*360*t) and

    the values shown.g. Click Apply.

    h. Click OK on the table.

    i. Click Apply.

    a

    b

    c

    d

    e

    f

    gh

    i

    Note the PCL Syntax:

    Sind Sine function in degrees

    t time is a Patran global variable

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    WS3-9NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 2. Field: Create / Non Spatial / Tabular Input (Cont.)

    Create a Non Spatial field forthe force load.

    a. Enterforce for theField Name.

    b. Select Time (t) as theActive IndependentVariable.

    c. Click Input Data.

    d. Click Map Functionto Table.

    e. Type in the function,-sind(250*360*t) andthe values shown.

    f. Click Apply.

    g. Click OK on the table.

    h. Click Apply.

    a

    b

    c

    d

    e

    f

    g

    h

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    WS3-10NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 3. Load Cases: Create

    Create a Time Dependent load case.

    a. Load Cases: Create.

    b. Enterdirect_transient for theLoad Case Name.

    c. Select Time Dependent asthe Load Case Type.

    d. Click Assign/Prioritize

    Loads/ BCs.

    e. Click on the Displ_constraint

    in the Select IndividualLoads/BCS field.

    f. Click OK.

    g. Click Apply.

    a

    b

    c

    d

    e

    f

    g

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    WS3-11NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 4. Loads/BCs: Create / Force / Nodal

    Create the time dependentForce load.

    a. Loads/BCs: Create /Force / Nodal.

    b. Enter50lb for theNew Set Name.

    c. Click on the InputData button.

    d. Enter forForce, and selectForce for theTime/Freq.Dependent Field.

    e. Click OK.

    f. Click on SelectApplication Region.

    g. Change the GeometryFilter to FEM.

    h. Select the bottom

    right corner node forthe application region.

    i. Click Add, and clickOK.

    j. Click Apply.

    a

    b

    c

    d

    e

    f

    g

    h

    i

    j

    i

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    WS3-12NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 5. Loads/BCs: Create / Pressure / Element Uniform

    Create the time dependentPressure load.

    a. Loads/BCs: Create /Pressure / ElementUniform.

    b. Enterpressure forthe New Set Name.

    c. Change the TargetElement Type to 2D.

    d. Click on the InputData button.

    e. Enter-1 for Top SurfPressure, and selectPressure for theTime/Freq.Dependent Field.

    f. Click OK.g. Click on Select

    Application Region.

    h. Select all theelements for theapplication region.

    i. Click Add, and clickOK.

    j. Click Apply.

    a

    b

    c

    d

    e

    f

    g

    h

    i j

    i

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    WS3-13NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 6. Analysis: Analyze / Entire Model / Full Run

    Submit the model for analysis.

    a. Analysis: Analyze /Entire Model / Full Run.

    b. Click on Solution Type.

    c. Select TransientResponse.

    d. Change the Formulationto Direct.

    e. Click on SolutionParameter.

    f. Enter 0.00259 for Wt-Mass Conversion.

    g. Enter0.06 for Struct.Damping Coefficientand 1570 for W3,Damping Factor.

    h. Click OK.

    i. Click OK.

    a

    b

    c

    d

    e

    f

    g

    h

    i

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    WS3-14NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 6. Analysis: Analyze / Entire Model / Full Run (Cont.)

    Submit the model for analysis(cont.).

    a. Click on Subcases.

    b. Select direct_transient

    from the AvailableSubcases field.

    c. Click on SubcaseParameters.

    d. Click on DEFINE TIMESTEPS button.

    e. Change Delta-T to0.0004. Click Enter.

    f. Click OK.

    g. Click OK.

    h. Click Apply.i. Click Cancel.

    a

    c

    b

    d

    e

    f

    g

    h i

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    WS3-15NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 6. Analysis: Analyze / Entire Model / Full Run (Cont.)

    Submit the model for analysis(cont.).

    a. Click on SubcaseSelect.

    b. Select direct_transient

    and unselect Default.

    c. Click OK.d. Click Apply.

    a

    b

    c

    d

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    WS3-16NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 7. Analysis: Access Results / Attach XDB / Result Entities

    Attach the XDB result file.

    a. Analysis: AccessResults / Attach XDB /Result Entities.

    b. Click on Select ResultsFile.

    c. Select ws3.xdb.d. Click OK.

    e. Click Apply.

    a

    b

    c

    d

    e

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    WS3-17NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 8. Results: Create / Graph / Y vs X

    Create a X-Y graph ofdisplacement results.

    a. Results: Create / Graph / Yvs X.

    b. Click onSC1:DIRECT_TRANSIENT.

    c. Select Global Variable asthe Filter Method.

    d. Click Filter.

    e. Click Apply.

    f. Click Close.

    a

    b

    c

    d

    e f

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    WS3-18NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 8. Results: Create / Graph / Y vs X (Cont.)

    Create a X-Y graph ofdisplacement results (cont.).

    a. Select Displacement,Translational for theSelect Y Result field.

    b. Select Z Component asthe Quantity.

    c. Click on the TargetEntities icon.

    d. Change the TargetEntity Selection toNodes.

    e. Select the upper right

    node (node oppositewhere force is applied).

    f. Click Apply.

    b

    a

    c

    d

    e

    f

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    WS3-19NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation

    Step 8. Results: Create / Graph / Y vs X (Cont.)

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    WS3-20NAS122, Workshop 3, August 2005Copyright 2005 MSC.Software Corporation