Conceptual Study on Hypersonic Airplanes using Pre-Cooled Turbojet-Reference-Cited by-同舟云学术

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Conceptual Study on Hypersonic Airplanes using Pre-Cooled Turbojet

Published:2008-04-28 Issue: Volume: Page:
ISSN:
Container-title:15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Taguchi Hideyuki¹,Murakami Akira¹,Sato Tetsuya²,Tsuchiya Takeshi³

Affiliation:

1. Japan Aerospace Exploration Agency

2. Waseda University

3. University of Tokyo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2503

Reference11 articles.

1. JAXALong-TermVision-JAXA2005-2005.

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2. A review of design issues specific to hypersonic flight vehicles;Progress in Aerospace Sciences;2016-07

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4. Combined-Cycle Engines;Encyclopedia of Aerospace Engineering;2010-12-15

5. An Experimental Study on Aerodynamic Design of Hypersonic Airplane;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14

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