Influence Parameter Analysis and Wrinkling Control of Space Membrane Structures-Reference-Cited by-同舟云学术

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Influence Parameter Analysis and Wrinkling Control of Space Membrane Structures

Published:2009-12-29 Issue:1 Volume:17 Page:49-59
ISSN:1537-6494
Container-title:Mechanics of Advanced Materials and Structures
language:en
Short-container-title:Mechanics of Advanced Materials and Structures

Author:

Wang C. G.,Mao L. N.,Du X. W.,He X. D.

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science,General Mathematics,Civil and Structural Engineering

Link

http://www.tandfonline.com/doi/pdf/10.1080/15376490903082862

Reference27 articles.

1. Blandino, J. R., Johnston, J. D., Miles, J. J. and Soplop, J. S. Thin Film Membrane Wrinkling due to Mechanical and Thermal Loads. Proceeding of the 42th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference. April16–19, Seattle, WA. AIAA 2001–1345

2. Kukathasan, S. and Pellegrino, S. Nonlinear Vibration of Wrinkled Membranes. Proceeding of the 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference. April7–10, Norfolk, Virginia. AIAA 2003–1747

3. Jenkins, C. H., ed. 2001.Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space Applications, vol. 191, Progress in Astronautics and Aeronautics, 103–105. 321–331. Reston, VA: AIAA.

4. An algorithm for finite element analysis of partly wrinkled membranes

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