Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition-Reference-Cited by-同舟云学术

Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition

Published:2005-05-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
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Author:

Takahashi Masahiro¹,Sunami Tetsuji¹,Tanno Hideyuki¹,Komuro Tomoyuki¹,Kodera Masatoshi¹,Itoh Katsuhiro¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3350

Reference5 articles.

1. 2Itoh, K. "Study on Scramjet Engine Characteristics under Mach 8 to 15 Conditions,'' Proceedings of the Fifth European Symposium onAerothermodynamics for SpaceVehicles, 2005(tobe appeared).

2. Aerodynamic force measurement on a large-scale model in a short duration test facility

3. Lordi, J. A., Mates, R. E., and Moselle, J. R. "Computer Program for the Numerical Solution of Nonequilibrium Expansionsof Reacting GasMixtures,'' NASA CR-472, 1966.

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