Ws06_modalfrequency

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    WS6-1

    WORKSHOP 6

    MODAL FREQUENCY RESPONSEANALYSIS

    NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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    WS6-2NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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    WS6-3NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

    MODAL FREQUENCY RESPONSE

    Problem Description Using the Modal Method, determine the frequency response of the

    flat rectangular plate, created in Workshop 1a, excited by a 0.1 psi

    pressure load over the total surface of the plate and a 1.0 lb. force

    at a corner of the tip lagging 45r. Use a modal damping of \ =

    0.03. Use a frequency step of 20 Hz between a range of 20 and

    1000 Hz; in addition, specify five evenly spaced excitationfrequencies between the half power points of each resonant

    frequency between the range of 20-1000 Hz.

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    WS6-4NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

    MODAL FREQUENCY RESPONSE

    P

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

    contains the loads and boundary constraints.

    1.0

    0.1 psi. over the total surface

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    WS6-5NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

    MODAL FREQUENCY 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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    WS6-6NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

    CREATE NEW DATABASE

    Create a new database calledws6.db.

    a. File / New.

    b. Enterws6 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

    b c

    d

    e

    f

    g

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    WS6-7NAS122, Workshop 6, 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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    WS6-8NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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

    Create a Non Spatial field forthe pressure load.

    a. Field: Create / NonSpatial / TabularInput.

    b. Enterpressure forthe Field Name.

    c. Select Frequency (f)

    as the ActiveIndependent Variable.

    d. Click Input Data.

    e. Enter the valuesshowed in the table.

    f. Click OK.

    g. Click Apply.

    a

    b

    c

    d

    e

    f

    g

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    WS6-9NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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

    Create a Non Spatial field forthe force load.

    a. Field: Create / NonSpatial / TabularInput.

    b. Enterforce for theField Name.

    c. Select Complex asthe Scalar Field Type.

    d. Click Input Data.

    e. Change the ComplexData Format toMagnitude-Phase

    (degrees).

    f. Enter the values

    showed in the table.g. Click OK.

    h. Click Apply.

    a

    bc

    d

    e

    f

    h

    g

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    WS6-10NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

    Step 3. Load Cases: Create

    Create a Time Dependent load case.

    a. Load cases: Create

    b. Entermodal_freq_response

    for the Load 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. b

    c

    d

    e

    f

    g

    a

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    WS6-11NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

    Step 4. Loads/BCs: Create / Force / Element Uniform

    Create the time dependentForce load.

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

    b. EnterForce for the NewSet Name.

    c. Click on the Input Data

    button.

    d. Enter for Force,and select force for theTime/Freq. DependentField.

    e. Click OK.

    f. Click on SelectApplication Region.

    g. Change the Geometry

    Filter to FEM.h. Select the node on the

    bottom right corner.

    i. Click Add, and click OK.

    j. Click Apply.

    a

    b

    c

    d

    e

    f

    g

    h

    j

    i

    i

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    WS6-12NAS122, Workshop 6, 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 for theNew Set Name.

    c. Change the TargetElement Type to 2D.

    d. Click on the Input Data

    button.

    e. Enter-0.1 for Top SurfPressure, and selectpressure for theTime/Freq. DependentField.

    f. Click OK.g. Click on Select

    Application Region.

    h. Select all the elementsfor the application region.

    i. Click Add, and click OK.

    j. Click Apply.

    a

    b

    c

    d

    e

    f

    g

    h

    i

    j

    i

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    WS6-13NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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

    Submit the model for analysis.

    a. Analysis: Analyze / EntireModel / Full Run.

    b. Click on Solution Type.

    c. Select FrequencyResponse.

    d. Change the Formulation toModal.

    e. Click on SolutionParameterbutton.

    f. Select Coupledfor MassCalculation.

    g. Enter0.00259 for Wt-MassConversion.

    h. Click OK.

    i. Click OK.

    a

    b

    c

    d

    e

    f

    h i

    g

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    WS6-14NAS122, Workshop 6, 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. Selectmodal_freq_response

    from the AvailableSubcases field.

    c. Click on SubcaseParameters.

    d. Click on DEFINE

    FREQUEYNCIES

    button.

    e. Use the values in the

    table.

    f. Click OK.

    a

    b

    c

    d

    e

    f

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    WS6-15NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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

    Submit the model for analysis(cont.).

    a. Change Modal Damping toCrit. Damping (CRIT).

    b. Click on DEFINE MODALDAMPING.

    c. Enter the values showed inthe Define Dampingwindow.

    d. Click OK.

    e. Click OK.

    f. Click Apply (on theSubcase form).

    g. Click Cancel.

    a

    b

    c

    d

    e

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    WS6-16NAS122, Workshop 6, 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. Selectmodal_freq_response

    and unselect Default.

    c. Click OK.

    d. Click Apply.

    a

    b

    c

    d

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    WS6-17NAS122, Workshop 6, 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 ResultFile.

    c. Select ws6.xdb

    .d. Click OK.

    e. Click Apply.

    a

    b

    c

    e

    d

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    WS6-18NAS122, Workshop 6, 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 / Y vs X.

    b. Click onSC1:MODAL_FREQ_

    RESPONSE.

    c. Select GlobalVariable as the FilterMethod.

    d. Click Filter.

    e. Click Apply.

    f. Click Close.

    a

    b

    c

    d

    e f

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    WS6-19NAS122, Workshop 6, 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 node where

    force is applied.

    f. Click Apply.

    b

    a

    c

    d

    e

    f

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    WS6-20NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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

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

    a. Click on DisplayAttribute.

    b. Change Y Axis Scalefrom Linear to Log.

    c. Click on Plot Option.

    d. Change the ComplexNo. as to Magnitude.

    e. Click Apply.

    b

    ac

    d

    e

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    WS6-21NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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

    Displacement Magnitudevs. Frequency Plot

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    WS6-22NAS122, Workshop 6, August 2005Copyright 2005 MSC.Software Corporation

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

    Create a X-Y graph of phase

    results.

    a. Change Complex No.as from Magnitude toPhase.

    b. Change Y Axis Scalefrom Log to Linear.

    c. Click Apply.

    a

    b

    a