Structural dynamic and aeroelastic considerations for hypersonic vehicles
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1255
Reference1 articles.
Cited by 7 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
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2. A reduced order aerothermodynamic modeling framework for hypersonic vehicles based on surrogate and POD;Chinese Journal of Aeronautics;2015-10
3. Modeling of Fuel Sloshing and its Physical Effects on Flutter;AIAA Journal;2013-09
4. Thermoelastic Analysis of an Heterogeneous Orthotropic Nose Cap for a Hypersonic Vehicle;Advanced Materials Research;2011-09
5. Aerothermoelastic Modeling Considerations for Hypersonic Vehicles;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14
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