nas120 ws02 simple beam

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WORKSHOP 2 SIMPLY SUPPORTED BEAM

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WORKSHOP 2

SIMPLY SUPPORTED BEAM

WS2-2NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

WS2-3NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Workshop ObjectivesA finite element model must be properly constrained to prevent rigid body motion. This workshop demonstrates what happens when a model is not adequately constrained.

WS2-4NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Problem DescriptionAnalyze a simply-supported beam with a concentrated loadBeam dimension 1” x 1” x 12”E = 30 x 106 psi ν =0.3Load = 200 lb

PP

WS2-5NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Suggested Exercise Steps1. Create a new database and name it inadequate_constraint.db. 2. Create a solid to represent the beam.3. Mesh the solid to create 3D elements. 4. Create in-plane boundary conditions.5. Apply loads.6. Create material properties. 7. Create physical properties.8. Run analysis with MSC.Nastran.9. View fatal errors in the .f06 file.10. Add new boundary condition to properly constrain model.11. Re-run the analysis. View the .f06 file.12. Access the results file.13. Plot results.

WS2-6NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

b c

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Step 1. Create New Database

Create a new database called inadequate_constraint.db

a. File / New.b. Enter

inadequate_constraintas the file name.

c. Click OK.d. Choose Tolerance Based

on Model.e. Select MSC.Nastran as

the Analysis Code.f. Select Structural as the

Analysis Type. g. Click OK.

a

e

WS2-7NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 2. Create Geometry

Create a solida. Geometry: Create / Solid /

Primitiveb. Enter 12 for the X Lengthc. Click Apply.d. Change to iso 1 view

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WS2-8NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

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Step 3. Mesh the Solid

Create a solid mesha. Elements: Create / Mesh /

Solidb. Screen pick the solidc. Click Apply.

WS2-9NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

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Step 4. Create Boundary Conditions

Create a boundary conditiona. Loads/BCs: Create /

Displacement / Nodal.b. Enter left_end as the

New Set Name.c. Click Input Data.d. Enter <0,0, > for

Translations. e. Click OK.

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c

a

WS2-10NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Apply the boundary conditiona. Click Select

Application Region.b. For the Geometry

Filter select Geometry.

c. Select the curve filterd. Screen pick the left

edge as showne. Click Add.f. Click OK. g. Click Apply.

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Step 4. Create Boundary Conditions

c

Screen pick this lower edgef

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WS2-11NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 4. Create Boundary Conditions

Create another boundary condition

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

b. Enter right_end as the New Set Name.

c. Click Input Data.d. Enter < ,0, > for

Translations. e. Click OK.

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e

b

a

c

WS2-12NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Apply the boundary conditiona. Click Select Application Region.b. For the Geometry Filter select

Geometry.c. Select the curve filterd. Screen pick the right edge as showne. Click Add.f. Click OK. g. Click Apply.

ed

b

Step 4. Create Boundary Conditions

c

Screen pick this edge

f

a

g

WS2-13NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 5. Apply Load

Create a loada. Loads/BCs: Create / Force

/ Nodal.b. Enter load as the New Set

Name.c. Click Input Data.d. Enter <0 -100 0> for Force. e. Click OK.

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c

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WS2-14NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Apply the loada. Click Select

Application Region.b. For the Geometry

Filter select FEM.c. Shift/pick the two

nodes as shownd. Click Add.e. Click OK. f. Click Apply.

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Step 5. Apply Load

cScreen pick these nodes

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f

WS2-15NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 6. Create Material Properties

Create an isotropic materiala. Materials: Create / Isotropic

/ Manual Input.b. Enter steel for the Material

Name.c. Click Input Properties.d. Enter 30e6 for the Elastic

Modulus.e. Enter 0.3 for the Poisson

Ratio.f. Click OK. g. Click Apply.

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WS2-16NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 7. Create Physical Properties

Create physical propertiesa. Properties: Create / 3D /

Solidb. Enter solid_beam as the

Property Set Name.c. Click Input Properties.d. Click on the Select

Material Icon.e. Select steel as the material

property name.f. Click OK.

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WS2-17NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Apply the physical propertiesa. Click in the Select

Members box.b. Screen pick the solidc. Click Add.d. Click Apply.

ac

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Step 7. Create Physical Properties

b

WS2-18NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 8. Run Linear Static Analysis

Analyze the modela. Analysis: Analyze /

Entire Model / Full Run.

b. Click Solution Type.c. Choose Linear Static

as the Solution Type.d. Click OK.e. Click Apply.

c

d

a

b

e

WS2-19NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 9. View F06 File

Examine the .f06 filea. Open the file titled

inadequate_constraint.f06 with any text editor.

b. Examine the warning and fatal messages.

Why has the job failed?a. The warning message in the .f06 file lists T3 as the

problem degree of freedom.b. With constraints in the x-y plane only, the beam has a

rigid body motion in the z direction. Need to add a constraint in the z direction.

WS2-20NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 10. Add New Boundary Condition

Add a boundary conditiona. Loads/BCs: Create /

Displacement / Nodal.b. Enter z_constraint as the

New Set Name.c. Click Input Data.d. Enter < , ,0 > for

Translations. e. Click OK.

d

e

b

c

a

WS2-21NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Apply the boundary conditiona. Click Select Application

Region.b. For the Geometry Filter

select Geometry.c. Select the point filterd. Screen pick the left corner

as showne. Click Add.f. Click OK. g. Click Apply.

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Step 10. Add New Boundary Condition

c

Screen pick this point

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WS2-22NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 11. Re-run Linear Static Analysis

Analyze the modela. Analysis: Analyze /

Entire Model / Full Run.

b. Click Solution Type.c. Choose Linear Static

as the Solution Type.d. Click OK.e. Click Apply.

After the analysis is completed, view the .f06 file to make sure there is no warning or fatal error message.

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d

a

b

e

WS2-23NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 12. Access the Results File

Access the results filea. Analysis: Access Results /

Attach XDB / Result Entities.b. Click Select Results File.c. Select the file

inadequate_constraint.xdbd. Click OK.e. Click Apply.

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WS2-24NAS120, Workshop 2, May 2006Copyright© 2005 MSC.Software Corporation

Step 13. Plot the Results

Plot the resultsa. Results: Create / Quick Plotb. Select Stress Tensor for

fringe resultc. Select Displacement,

Translational for deformation result

d. Click Apply.

-- End of workshop --

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