The case for explicit finite element analysis of fabric systems - A presentation of real world applications
Author:
Affiliation:
1. Irvin Aerospace, Inc., Santa Ana, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2002
Reference9 articles.
1. Taylor,A.P.,andDelurgio,P.R."An Overviewof the Landing System for the K-l Launch Vehicle, ParachutesandAirbags"AIAA97-1515
2. Gardinier, D. and Taylor, A.P. "Design and Testing of the K-l Reusable Launch Vehicle Landing System Airbags"AIAA 99-1757
3. Taylor, A.P., Benney, R. and Bagdonovich, B. "Investigation Of The Application Of Airbag Technology ToProvideA Soft Landing Capability For Military Heavy Airdrop"AIAA2001-2045
Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. FLOATSTAB - A Tool for the Rapid Analysis of Flotation Stability Following Water Landing;18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2005-05-23
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