An Experimental Study on Aerodynamic Design of Hypersonic Airplane-Reference-Cited by-同舟云学术

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An Experimental Study on Aerodynamic Design of Hypersonic Airplane

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

Nakatani Hiroki¹,Taguchi Hideyuki²,Hongoh Motoyuki²,Honami Shinji¹

Affiliation:

1. Tokyo University of Science

2. Japan Aerospace Exploration Agency (JAXA)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-7434

Reference9 articles.

1. JAXALongTermVision,March2005,URL:http://www.jaxa.jp/about/2025/pdf/2025_02.pdf,(inJapanese).

2. Conceptual Study on Hypersonic Airplanes using Pre-Cooled Turbojet

3. Design Study on a Small Pre-Cooled Turbojet Engine for Flight Experiments

4. Taguchi, H., Fujita, K., Shindo, S., Tsuda, S., Hirabayashi, N., Koyama, T. and Ito, R. "Mach 5 Wind Tunnel Test of HypersonicAirplane",JAXA-RR-07-047,2008.(in Japanese).

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. Evaluation of Aerodynamic Performance of a Hypersonic Experimental Aircraft;17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2011-04-11

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