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WS4-1
WORKSHOP 4
MODAL TRANSIENT ANALYSIS
NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
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WS4-2NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
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WS4-3NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
Problem Description Using the Modal Method, determine the transient response of the
flat rectangular plate, created in Workshop 3, subject to time-
varying excitation. This example structure is excited by a 1 psi
pressure load over the total surface of the plate varying at 250 Hz.
In addition, a 25 lb force is applied at a corner of the tip also
varying at 250 Hz, but starting 0.004 seconds after the pressureload begins. Both time-dependent dynamic loads are applied for
the duration of 0.008 seconds only. Use a modal damping of z =
0.03 for all modes. Carry out the analysis for 0.04 seconds.
MODAL TRANSIENT RESPONSE
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WS4-4NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
Problem Description (cont.) Below is a finite element representation of the flat plate. It also
contains the loads and boundary constraints.
MODAL TRANSIENT RESPONSE
X
Y
Z
12345
25.0
12345
12345
12345
12345
1.0 psi o ver the total surface
X
Y
Z
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WS4-5NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
MODAL 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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WS4-6NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
CREATE NEW DATABASE
Create a new database calledws4.db.
a. File / New.
b. Enter ws4 as the file name.
c. Click OK.
d. Choose Default Tolerance.
e. Select MSC.Nastran as the Analysis Code.
f. Select Structural as the Analysis Type.
g. Click OK.
a
b c
d
e
f
g
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WS4-7NAS122, Workshop 4, 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.
bc
a
d
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WS4-8NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
Step 2. Field: Create / Non Spatial / Tabular Input
Create a Non Spatial field for the pressure load.
a. Field: Create / NonSpatial / Tabular Input.
b. Enter pressure for the Field Name.
c. Select Time (t) as the Active IndependentVariable.
d. Click Input Data.
e. Click Map Function
to Table.
f. Type in the function,sind(250*360*¶t) and
values shown.g. Click Apply.
h. Click OK on the table.
i. Click Apply.
a
b
c
d
e
f
gh
i
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WS4-9NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
Step 2. Field: Create / Non Spatial / Tabular Input (Cont.)
Create a Non Spatial field for the force load.
a. Enter force for theField Name.
b. Select Time (t) as the Active IndependentVariable.
c. Click Input Data.
d. Click Map Function
to Table.
e. Type in the function,sind(250*360*(¶t-
0.004)) and values
shown.
f. Click Apply.
g. Click OK on the table.
h. Click Apply.
a
b
c
d
e
f
g
h
Note the required Delay has been
defined by putting in a start time of 0.004 and term (µt-0.004)
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WS4-10NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
Step 3. Load Cases: Create
Create a Time Dependent load case.
a. Load Cases: Create
b. Enter modal_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
e
f g
d
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WS4-11NAS122, Workshop 4, 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. Enter force for theNew Set Name.
c. Click on the Input
Data button.
d. Enter <0 0 25> for Force, and selectForce for theTime/Freq.Dependent Field.
e. Click OK.
f. Click on Select
Application Region.
g. Change the GeometryFilter to FEM.
h. Select the bottom
right corner node for the 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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WS4-12NAS122, Workshop 4, 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. Enter pressure for the New Set Name.
c. Change the TargetElement Type to 2D.
d. Click on the Input
Data button.
e. Enter -1 for Top Surf Pressure, 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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WS4-13NAS122, Workshop 4, 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 Transient
Response.
d. Change the Formulationto Modal.
e. Click on Solution
Parameter button.
f. Enter 0.00259 for Wt-Mass Conversion.
g. Click OK.
h. Click OK.
a
b
c
d
e
f
g
h
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WS4-14NAS122, Workshop 4, 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 modal_transient
from the AvailableSubcases field.
c. Click on Sub
caseParameters.
d. Click on DEFINE TIME
STEPS button.
e. Change Delta-T to0.0004. Click Enter.
f. Click OK.
a
b
c
d
e
f
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WS4-15NAS122, Workshop 4, 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 MODAL
DAMPING.
c. Enter the values showed inthe Define Dampingwindow.
d. Click OK.
e. Click OK.
f. Click Apply (on theSubcases form).
g. Click Cancel.
a
b
c
d
e
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WS4-16NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
Step 6. Analysis: Analyze / Entire Model / Full Run (Cont.)
Submit the model for analysis(cont.).
a. Click on Subcase
Select.
b. Select modal_transient
and unselect Default.
c. Click OK.d. Click Apply.
a
b
c d
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WS4-17NAS122, Workshop 4, 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 Result
File.
c. Select ws4.xdb
.d. Click OK.
e. Click Apply.
a
b
c
d
e
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WS4-18NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
Step 8. Results: Create / Graph / Y vs X
Create a X-Y graph of displacement results.
a. Results: Create / Graph / Yvs X.
b. Click onSC1:MODAL_TRANSIENT.
c. SelectGlobal Variable
asthe Filter Method.
d. Click Filter .
e. Click Apply.
f. Click Close.
a
b
c
d
e f
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WS4-19NAS122, Workshop 4, August 2005Copyright¥ 2005 MSC.Software Corporation
Step 8. Results: Create / Graph / Y vs X (Cont.)
Create a X-Y graph of displacement results (cont.).
a. Select Displacement,
Translational for theSelect Y Result field.
b. Select Z Component asthe Quantity.
c. Click on the Target
Entities icon.
d. Change the TargetEntity Selection toNodes.
e. Select the upper right
node. Also choose thenode at the center of the
free edge.f. Click Apply.
b
a
c
d
e
f