Tube Creep

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    WORKSHOP 4

    Creep of a Steel Tube

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    Model Description

    In this exercise, we simulate the creep behavior of a stainless steel ovaltube pressurized at high temperature. Using symmetry, only half the tube

    is modeled with plane strain elements.

    The material constitutive behavior has the creep strain rate dependent

    upon the stress level (Norton Creep). The material data has been fitted

    with a power relation where the creep strain rate is expressed as:

    Oval tube will bulge and become a completely circular over time, and will

    rupture due to the large strains.

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    Exercise Overview:

    Build the tube geometry and mesh from a session file. Create the Boundary Conditions.

    Create the Pressure Load.

    Create the Material Properties.

    Create the Element Properties. Set up and Submit the job to analysis.

    Evaluate the results.

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    Step 1: Open a New Database

    Open a new database namedtube.db:

    a. File > New.

    b. Type tubeas File name.

    c. Click OK.

    d. Click OK to select MD

    Nastran as the AnalysisCode. db c

    a

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    When the session file is done the viewport will contain all

    the geometry and the FE Mesh of a section of the tube.

    Step 2. Run the Provided Session File

    a

    Run the provided session file.

    a. Select File / Session /

    Play.

    b. Select

    tube_model.ses as

    the File name.

    c. Click Apply.

    (This action will run the

    session file. Please do

    not interrupt it.)

    b

    c

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    Step 3. Create the Symmetry Boundary Condition

    Create the Symmetry Boundary

    Condition.

    a. Loads/BCs: Create /

    Displacement /

    Nodal.

    b. EnterSymmetry_X as

    the New Set Name.

    c. Click on Input Data.

    d. Enter for the

    Translation.

    e. Click OK.

    d

    e

    a

    b

    c

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    g

    f. Click on Select

    Application

    Region.

    g. Select the Curve or

    Edge icon.

    h. Select the two edges

    along the y-axis

    i. Click Add.

    j. Click OK.

    k. Click Apply.

    Step 3. Create the Symmetry Boundary Condition (Cont.)

    f

    k

    i

    j

    h

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    Step 4. Create a constraint in the vertical (Y) direction

    a. EnterFix_Y as the

    New Set Name.

    b. Click on Input Data.

    c. Enter for theTranslation.

    d. Click OK.

    c

    d

    Fix a node in the Y direction, to prevent rigid

    body motion

    a

    b

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    e. Click on Select

    Application Region

    f. Change the Select

    Filter to FEM.

    g. Select any node from

    the y-symmetry line.

    h. Click Add.

    i. Click OK.

    j. Click Apply.

    Step 4. Create the Symmetry Boundary Conditions

    gh

    f

    ie

    j

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    Step 5. Create the pressure load

    a. Loads/BCs: Create / Pressure

    / Element Uniform

    b. EnterPressure as the New

    Set Name.

    c. Select 2D as Target ElementType

    d. Click on Input Data.

    e. Enter66 forEdge Pressure.

    f. Click OK.

    a

    bc

    d

    e

    f

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    g. Click on Select

    Application Region.

    h. Change the Select

    Filter to Geometry.

    i. Select the Edge icon.

    j. Select the four inner

    edges.

    k. Click Add.

    l. Click OK.

    m. Click Apply.

    g

    Step 5. Create the pressure load (Cont.)

    m

    i

    k

    l

    j

    h

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    Step 6: Create the Material

    To create an isotropic creep material:

    a. Materials: Create Isotropic >Manual Input.

    b. EnterStainless_Steel forMaterialName.

    c. Click Input Properties.d. Enter21.4E6forElastic Modulus.

    e. Enter0.3 forPoisson Ratio.

    f. Click OK.

    g. Click Apply.

    a

    de

    f

    a

    b

    c

    g

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    Step 6: Create the Material (Cont.)

    h. Click on Input Properties

    i. Select Creep as Constitutive Model

    j. Select MATVP forCreep Data Input

    k. Enter4.E-24forCoefficient.

    l. Enter4.51 forExponent of Stress.

    m. Click OK.n. Click Apply.

    h

    i

    j

    k

    l

    mn

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    Step 7: Apply Properties

    To apply properties:

    a. Properties: Create

    > 2D > 2D Solid.

    b. Entertube for

    Property Set Name.

    c. Select Plain

    Strain, and

    Standard

    Formulation.

    d. Click Input

    Properties.

    e. Click the Select

    Material icon.

    f. Select

    Stainless_Steel.

    g. Click Ok.

    a

    a

    c

    d

    b

    ef

    g

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    Step 7: Apply Properties (Cont.)

    h. Click Select

    Application

    Region.

    i. Click in the

    Select Members

    text box.

    j. Select all thesurfaces.

    k. Click Add.

    l. Click Ok.

    m. Click Apply.

    h

    i

    k

    l

    m

    j

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    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck

    Set up the non-linear Analysis job.

    a. Analysis: Analyze / Entire

    Model / Analysis Deck.

    b. Entertube as the Job Name.

    c. Open Solution Type.

    d. Select Implicit NonlinearasSolution Type.

    e. Click on Solution

    Parameters

    f. Check SOL400 Run,and

    Assumed Strain

    g. Click on Results Output

    Formate

    d

    a

    f

    f

    g

    b

    a

    c

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    h. Select XDB

    i. Select Print

    j. Click OK.

    k. Click OK.

    l. Click OK.

    h i

    j

    k

    l

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    m. Click on Subcases

    n. Click on Default under

    Available Subcases

    o. Enterstep_1_static as

    Subcase Name

    p. Click on SubcaseParameters.

    q. Select Large

    Displacement/Large

    Strains.

    r. Click on Load Increment

    Parameters

    q

    n

    o

    pr

    m

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    s. Select Fixed

    t. Enter1as Number of

    Increments

    u. Click OK.

    v. Click on Iteration

    Parameters

    v

    s

    t

    u

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    w. Select Pure Full Newton

    as Matrix Update Method

    x. Enter4as Max # of

    Bisections

    y. Click OK.

    z. Click OK.

    z

    w

    x

    y

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    aa. Click on Output Requests

    bb. Click on Standard Output

    cc. Select Element Strains

    dd. Select Non-Linear Stress

    ee. Click OK

    ff. Click OKgg. Click Apply

    bb

    cc

    dd

    eeff gg

    aa

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    hh. Enterstep_2_creep as

    Subcase Name

    ii. Select Creep as Analysis

    Type

    jj. Click on Subcase

    Parameters.kk. Select Explicit Creep as

    Procedure

    ll. Click on Load Increment

    Parameters

    hh

    ii

    jj

    kk

    ll

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    mm. Select Adaptive Creep

    nn. Enter17.35as Suggested

    Time Increment

    oo. Enter3.47E6 as Total Time

    pp. Enter9999as Max. #

    Number of Increments

    Allowed

    qq. Click OK.

    rr. Click OK

    mmnn

    oo

    pp

    qq

    rr

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    ss. Click Apply

    tt. Click Cancel

    ss tt

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    uu. Clickon Subcase Select

    vv. Selectstep_1_Static, and

    Step_2_Creep

    ww. UnselectDefault

    xx. Click OK

    yy. Click Apply

    uu

    vv

    ww

    xx

    yy

    Step 8. Set up Analysis: Analyze / Entire Model / Analysis Deck (Cont.)

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    Step 9. Edit the exported input file

    Edit the file, tube.bdf (be sure to save it when done):

    a. Replace the following lines :

    by

    MDLPRM,REALT,1

    MDLPRM,NLDIAG,10

    NLMOPTS,CREEP

    ,LRGSTRN,1,

    NLPARM,1,1,1.e-9,PFNT, ,40,PV,

    ,0.01,0.01,

    NLPARM,2,200000,17.35,PFNT,,40,PV,YES

    ,0.01,0.01,

    ,10

    NLADAPT, 2

    , STEP, 0.1, 1.5, 1.0-8, 0.5, 999999, 6, 1.2

    , , 0, 2.-4,

    , CREEP, 0, 0.5, 1.0, 0.05

    PLPLANE, 1, 1

    PSHLN2, 1, 1, 1, 1.0,

    , C4, PLSTRN, L

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    Step 9. Edit the exported input file (Cont.)

    b. Replace the following line :

    by :

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    Step 10. Run MD Nastran

    Run MD Nastran with file, tube.bdf

    a. Double Click on the MD Nastran icon in the desktop

    b. Select tube.bdfas input File name

    c. Click Open

    d. Click Run (job might take 10+ minutes to run)

    a

    b

    c

    d

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    Read (Attach) results.

    a. Access Results / Attach XDB /

    Result Entities.

    b. Click on Select Results File ..

    c. Selecttube.xdb

    d. Click OK

    e. Click Apply.

    Step 11: Access the nonlinear Results

    aXV

    c

    d

    b

    e

    a

    St 12 Vi R lt

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    Step 12: View Results

    To create a fringe results plot:

    a. Results: Create > Quick Plot.

    b. Select thefirst Results case

    c. Select Logarithmic Strains, as the Fringe

    Resultd. Select Displacements, Translational.

    e. Click the Display Attributes icon.

    f. Change the Scale Interpretation to True Scale.

    g. Click Apply.

    f

    g

    a

    a

    b

    c

    d

    e

    St 12 Vi R lt (C t )

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    Step 12: View Results (Cont.)

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    Step 12 Vie Res lts (Cont )

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    k. Select thelast Results case

    l. Select Logarithmic Strains, as the Fringe Result

    m. Click Apply. k

    l

    m

    Step 12: View Results (Cont.)

    Step 12: View Results (Cont )

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    Step 12: View Results (Cont.)

    Step 12: View Results (Cont )

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    n. Select Cauchy Stresses as the Fringe Result

    o. Click Apply.

    n

    o

    Step 12: View Results (Cont.)

    Step 12: View Results (Cont )

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    Step 12: View Results (Cont.)

    Step 13 Quit Patran

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    Step 13. Quit Patran