Integrated aero-propulsive CFD methodology for the Hyper-X flight experiment-Reference-Cited by-同舟云学术

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Integrated aero-propulsive CFD methodology for the Hyper-X flight experiment

Published:2000-08-14 Issue: Volume: Page:
ISSN:
Container-title:18th Applied Aerodynamics Conference
language:
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Author:

Cockrell, Jr. Charles¹,Engelund Walter¹,Dilley Arthur²,Bittner Robert²,Jentink Tom²,Frendi Abdelkader³

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. FDC-NYMA, Inc., Hampton, VA

3. Alabama, Univ., Huntsville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4010

Reference20 articles.

Cited by 6 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. Propulsion Research and Academic Programs at the University of Alabama in Huntsville - 30th Anniversary Summary;AIAA Propulsion and Energy 2021 Forum;2021-07-28

3. Optimization of hypersonic aircraft using genetic algorithms;Applied Mathematics and Computation;2014-09

4. Hyper-X flight engine ground testing for X-43 flight risk reduction;10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference;2001-04-24

5. Hyper-X program status;39th Aerospace Sciences Meeting and Exhibit;2001-01-08

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