Geometrical effects to aerodynamic performance of scramjet engine-Reference-Cited by-同舟云学术

Geometrical effects to aerodynamic performance of scramjet engine

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
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Author:

Tani Kouichiro¹,Kanda Takeshi¹,Sunami Tetsuji¹,Hiraiwa Tetsuo¹,Tomioka Sadatake¹,Tani Kouichiro¹,Kanda Takeshi¹,Sunami Tetsuji¹,Hiraiwa Tetsuo¹,Tomioka Sadatake¹

Affiliation:

1. National Aerospace Lab., Kakuda, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3018

Reference15 articles.

1. Mach 4 testing of scramjet inlet models

2. Ishiguro,T., Ogawa,S., Wada,W. "Numerical Calculation of Scramjet Inlet Flow," NAL Technical Report TR-1174T, 1992

3. Ignition and Combustion Performance of Scramjet Combustors with Fuel Injection Struts

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