Structural dynamic and aeroelastic considerations for hypersonic vehicles-Reference-Cited by-同舟云学术

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Structural dynamic and aeroelastic considerations for hypersonic vehicles

Published:1991-04-08 Issue: Volume: Page:
ISSN:
Container-title:32nd Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

CAZIER, JR. F.¹,RICKETTS RODNEY¹

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

1. Transient Temperature Effects on the Aerothermoelastic Response of a Simple Wing;Aerospace;2018-07-02

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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