Wrinkling prediction of rectangular shell-membrane under transverse in-plane displacement

Author:

Wang C.G.,Tan H.F.,Du X.W.,Wan Z.M.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Modeling and Simulation

Reference17 articles.

1. A geometrically nonlinear finite element analysis of wrinkled membrane surface by a no-compression material model;Contri;Communication in Applied Numerical Methods,1988

2. Advances in the study of wrinkles in space membrane structures (in Chinese);Du;Journal of Advances in Mechanics,2006

3. Analysis of fabric tension structures;Fujikake;C&S,1989

4. Jenkins, C.H., (Ed.), 2001. Gossamer spacecraft: membrane and inflatable structures technology for space applications. In: Progress in Astronautics and Aeronautics, vol. 191. Published by the American Institute of Aeronautics and Astronautics, Inc., 1801 Alexander Bell Drive, Reston, VA 20191-4344. December 2000, pp. 103–105.

5. Jenkins, C.H., (Ed.), 2006. Recent advances in Gossamer Spacecraft. Progress in Astronautics and Aeronautics, vol. 212. Published by the American Institute of Aeronautics and Astronautics, Inc., 1801 Alexander Bell Drive, Reston, VA 20191-4344. September 2005, pp. 109–164.

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