Experimental approach to the HYPR Mach 5 ramjet propulsion system-Reference-Cited by-同舟云学术

Experimental approach to the HYPR Mach 5 ramjet propulsion system

Published:1998-07-13 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Ohshima Takao¹,Enomoto Yoshinari¹,Nakanishi Hidemasa²,Futamura Hisao³,Yanagi Ryoji³,Mitani Tohru⁴

Affiliation:

1. Kawasaki Heavy Industries, Ltd., Akashi, Japan

2. Mitsubishi Heavy Industries, Ltd., Aichi, Japan

3. National Aerospace Lab., Chofu, Japan

4. National Aerospace Lab., Kakuda, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3277

Reference7 articles.

1. Futamura, H., Enomoto, Y., Ohshima, T., Kimura, H., Fujiwara, K., Kinoshita, Y., Nakanishi, H., Mitani, T. and Yanagi,R. "FREEJET TEST OF RAMJET SYSTEM FOR HYPERSONIC TRANSPORT VEHICLE", ISABE97-7080,1997.

2. Control of the intake shock-position in the test rig for ramjet engine

3. Starting characteristics of supersonic inlets

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