Evaluation of Tension Field Theory for Wrinkling Analysis With Respect to the Post-Buckling Study
Author:
Affiliation:
1. University of Tokyo, Department of Aeronautics and Astronautics, Tokyo, Japan
2. Division of Spacecraft Engineering, The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai Sagamihara, Kanagawa 229-8510, Japan
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/71/4/532/5471230/532_1.pdf
Reference28 articles.
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3. Johnston, J., 2002, “Finite Element Analysis of Wrinkled Membrane Structures for Sunshield Applications,” Paper No. AIAA-2002-1456.
4. Blandino, J. R., Johnston, J. D., Miles, J. J., and Soplop, J. S., 2001, “Thin Film Membrane Wrinkling due to Mechanical and Thermal Loads,” Paper No. AIAA-2001-1345.
5. Roddeman, D. G., Drukker, J., Oomens, C. W. J., and Janssen, J. D., 1987, “Wrinkling of Thin Membranes: Part I—Theory; Part II—Numerical Analysis,” ASME J. Appl. Mech., 54, pp. 884–892.
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