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TECHNICAL PAPERS

An Iterative Method for Solving Elasticity Problems for Composite Laminates

[+] Author and Article Information
A. Makeev, E. A. Armanios

School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332-0150

J. Appl. Mech 67(1), 96-104 (May 18, 1999) (9 pages) doi:10.1115/1.321154 History: Received July 15, 1998; Revised May 18, 1999
Copyright © 2000 by ASME
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References

Figures

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Coordinate system and dimensions
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Shear stress distribution at the free edge x=b for orthotropic beam torsion. Comparison of one-term approximation with exact solution.
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Shear stress distribution at the free edge x=b for orthotropic beam torsion. Comparison of two-term approximation with exact solution.
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Shear stress distribution at the free edge x=b for orthotropic beam torsion. Comparison of three-term approximation with exact solution.
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Comparison of second iterations for one and two-term approximations with exact solution for orthotropic beam torsion
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One-term approximation. Comparison of stress predictions at +45/−45 ply interface for axial extension of [+45/−45]s laminate.
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One-term approximation. Comparison of stress predictions at +45/−45 ply interface for axial extension of [+45/−45]s laminate.
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Two-term approximation. Comparison of stress predictions at +45/−45 ply interface for axial extension of [+45/−45]s laminate.
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Two-term approximation. Comparison of stress predictions at +45/−45 ply interface for axial extension of [+45/−45]s laminate.
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Comparison of stress predictions at +45/−45 ply interface for axial extension of [+45/−45]s laminate
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Comparison of stress predictions at +45/−45 ply interface for axial extension of [+45/−45]s laminate
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Comparison of interlaminar shear stress predictions at the free edge for axial extension of [+45/−45]s laminate
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One-term approximation. Comparison of interlaminar shear stress predictions at the free edge x=b for torsion of [012/±302]s laminate.
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Two-term approximation. Comparison of interlaminar shear stress predictions at the free edge x=b for torsion of [012/±302]s laminate.

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