Lab Report Cae

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    Objective

    1) Familiarizing with MSC PATRAN & NASTRAN

    2) Building and analyzing simple solid geometry

    3) Checking structural integrity of simply supported beam

    Problem Statement

    Analyze a simple-supported beam with a concentrated load

    Beam dimension 1 x 1 x 12

    E = 30 x 106psi

    v= 0.3

    load = 200 lb

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    Methodology

    Step 1: Created a new database and name it as new1. Then chose based on model as the tolerance,

    selected MSC.Nastran as the analysis code and structural as the analysis type in the new model

    preferences.

    Step 2: Create a solid to represent the beam by clicked the icon geometry at the above. Next

    selected create, solid and primitive. Filled the length, x axis of the beam as 12 that given in the

    question and changed the solid into iso 1 view.

    Step 3: Chose the icon of element at the above to create a solid mesh and selected create, mesh

    and solid. After that, picked the solid that needed to fill in input list and apply it.

    Step 4: Selected the icon of load/BCs for the use of created boundary conditions. Picked create,

    displacement and nodal in first three choices and entered left_end as the new set name. Then

    clicked input data and entered for translations and clicked ok. After that, clicked select

    application region and selected geometry for geometry filter. Clicked the curve filter at the above

    and picked the left edge of the solid then clicked add, ok and apply.

    Repeated the step 4 by created another boundary condition but with for translations and

    with right edge of the solid.

    Step 5: Applied load which maintain with load/BCs and selected create, force and nodal. Entered

    load as the new set name. Then clicked input data and entered for force and clicked

    ok. Next, clicked select application region and selected FEM for the geometry filter. Shifted the

    two node at the middle of the solid, then clicked add, ok and apply.

    Step 6: Clicked Material for creating material properties and selected create, isotropic and

    manual input. Entered steel as the material name, clicked input properties and entered 30e6 for

    the elastic modulus and 0.3 for the poisson ratio. Lastly clicked ok and apply.

    Step 7: Clicked the properties icon to create physical properties. Selected create, 3D and solid

    and entered solid_beam as the property set name. Selected on steel in the input properties and

    clicked ok. After that, clicked on select members box and picked the solid and clicked add, apply.

    Step 8: Run analysis with MSC.Nastran by selected the analysis icon and clicked analyze, entire

    model, and full run. Next, clicked solution type and chose linear static as the solution type then

    continue with ok and apply.

    Step 9: Examined the warning and fatal error messages with opening of the file titled new1.f06

    with any text editor.

    Step 10: Add new boundary condition to properly constrain model. Clicked on load/BCs icon

    and selected create, displacement and nodal. Entered z_constraint as the new set name then

    clicked input data and entered < , ,0> for translations and clicked ok. Next, clicked select

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    application region and selected geometry for the geometry filter. Selected the point filter at the

    above and pick the left corner of the solid that same point in step4. Clicked add, ok and apply.

    Step 11: Re-run the analysis by repeated the step 8 and 9. Make sure that there is no warning or

    fatal error message in .f06 file.

    Step 12: Access the results file by selected access results, attach XDB and result entities. Clicked

    select result file and selected the file new1.xdb and clicked ok and apply.

    Step13: Clicked on icon result to plot the result. Chose create, quick plot. Then selected stress

    tensor for fringe result, displacement for deformation result and apply.

    Result

    a) fringe plot (deformed)

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    b) stress tensor only

    c) displacement only

    From MSC Nastran, it shown that the maximum stress is 3.46x103lb in

    -2and the minimum stress

    is 1.76x103lb in

    -2. The average stress is 2.61x10

    3lb in

    -2. The maximum displacement is

    2.95x10-3

    in

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    Discussion

    The analysis

    Conclusion/Summary