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TECHNICAL PAPERS

Evaluation of Tension Field Theory for Wrinkling Analysis With Respect to the Post-Buckling Study

[+] Author and Article Information
T. Iwasa

University of Tokyo, Department of Aeronautics and Astronautics, Tokyo, Japane-mail: taka@taurus.eng.isas.jaxa.jp

M. C. Natori, K. Higuchi

Division of Spacecraft Engineering, The Institute of Space and Astronautical Science, 3-1-1 Yoshinodai Sagamihara, Kanagawa 229-8510, Japan

J. Appl. Mech 71(4), 532-540 (Sep 07, 2004) (9 pages) doi:10.1115/1.1767171 History: Received May 01, 2003; Revised January 30, 2004; Online September 07, 2004
Copyright © 2004 by ASME
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References

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Figures

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Bird-eye view of a wrinkled membrane (structural scale: 500)
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Bird-eye view of a wrinkled membrane (structural scale: 2500)
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Nondimensional M–ϕ curves
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Out-of-plane displacement ratio of wrinkles
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Maximum amplitude ratio of wrinkles
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Location of maximum amplitude of wrinkles
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Wave of wrinkles at the radial location of r/b=0.83
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Comparison of nondimensional moment
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Angle of wrinkles (radial location: 0.4)
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Angle of wrinkles (radial location: 0.8)
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Comparison of strain energy ratio
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Strain energy ratio in wrinkled region
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Strain energy ratio in unwrinkled region
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Strain energy in wrinkled region with large compressive stress
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Strain energy in wrinkled region with small compressive stress
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Location of maximum amplitude of wrinkles and wrinkled region
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Mechanism of wrinkling behavior

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