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7/28/2019 Tube Creep
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WS4-1
NAS133-a, Workshop 4, March 2009
Copyright 2009 MSC.Software Corporation
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
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