Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted...
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Transcript of Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted...
![Page 1: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/1.jpg)
Modeling of Composite Tubes Using ANSYS
JEFF KAPKE
ME 450 Introduction to CAE
May 3, 2000
Submitted to: Professor H.U. Akay
![Page 2: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/2.jpg)
Uses for Composite Materials
• Aircraft
• Prosthetic Limbs
• Auto body
• Auto Frame
• Bridge Reinforcement
• Shafts and Rods
• Body Armour
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Advantages of Composites
• Density of aluminum alloy approximately 2800 kg/m3
• Density of carbon/epoxy approximately 1580 kg/m3
• Tensile strength of aluminum alloy 7075-T6 is 570 MPa
• Tensile strength of carbon/epoxy 1830 MPa
![Page 4: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/4.jpg)
Isotropic vs. Orthotropic
E
E
EE
E
E
E = E = E = E = E = E
E1
E2
Ey
Ex
Ex Ey E1 E2
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Fabrication
![Page 6: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/6.jpg)
Layers of a Composite Tube
Each color represents a different fiber orientation and change in material properties relative to the Global Axis.
X
![Page 7: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/7.jpg)
Modeled Tube in ANSYS
![Page 8: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/8.jpg)
Element Coordinate System Shell 91 From ANSYS Element Library
Theta
YZ
XI
L K
J
Ex
Ex
Element Type is SHELL91
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ANSYS Coordinate System for Shell Element
x
zy
z
x
y
zx
y
![Page 10: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/10.jpg)
ANSYS Element Coordinate System
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ANSYS Model SetupConstrained with Point Load
![Page 12: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/12.jpg)
ANSYS Model SetupConstrained with Uniform Load
![Page 13: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/13.jpg)
Real Test on Composite Tube
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Filament Wound Tube
![Page 15: Modeling of Composite Tubes Using ANSYS JEFF KAPKE ME 450 Introduction to CAE May 3, 2000 Submitted to: Professor H.U. Akay.](https://reader036.fdocuments.us/reader036/viewer/2022062715/56649db25503460f94aa2595/html5/thumbnails/15.jpg)
Deformed and Un-deformedPoint Load with 90o Fiber Orientation
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Von Mises PlotPoint Load 0o Orientation
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Von Mises PlotPoint Load/90o Orientation
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Von Mises Graph of 90o/Hoop Orientation
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Von Mises Graph of 0o/Longitudinal Orientation
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Von Mises Plots of Uniform Loading with Different Orientations
0o Orientation 90o Orientation
[0o,90o,45o]s
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Displacement of Point Loaded 90o/Hoop Orientation (Maximum Displacement 4.934mm)
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Displacement Related to Orientation
• Uniformly loaded hoop has greatest displacement.
• Combination of layers decreases displacement.
• Displacement related to stiffness.
0
1
2
3
4
5
6
Lo
ng
Pn
t
Ho
op
Pn
t
Lo
ng
Ho
op
[0,9
0,45
]s
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Results of Changing Orientation
• Hoop or 90o orientation is strong under transverse loading.
• Longitudinal or 0o orientation is stiffer in bending.
• Combination of orientations increases stiffness and strength.
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Difficulties with ANSYS
• Creating model is not straight forward and simple.
• Meshtool does not recognize that all element axis should coincide within each layer.
• ANSYS is too powerful for simple problems.
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Advantages of ANSYS
• Changing material properties or layer orientation is simple.
• Many different orientations can be analyzed in a short amount of time.
• ANSYS can predict results before fabricating composite sample.
• Complex geometries can be modeled and evaluated easily.
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New Ideas• Analyze tube in torsion.• Apply moment instead of load.• Test as a pressure vessel.• Model unique geometries and
compare results.• Model a beam or flat plate and
compare with actual results.