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8/6/2019 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