Scramjet Performance-Reference-Cited by-同舟云学术

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Scramjet Performance

Published:2001-01-01 Issue: Volume: Page:369-446
ISSN:
Container-title:Scramjet Propulsion
language:
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Author:

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/5.9781600866609.0369.0446

Reference192 articles.

1. 2Hicks,B.L."Addition ofHeat to a CompressibleFluid inMotion,"NACAACR E5A29,Feb.1945.

2. 3Perchonok, E., and Wilcox, F. A. "Investigation of Ramjet Afterburning as a Means ofVaryingEffective Exhaust Nozzle Area,"NACA RM E52H27,Nov.1952.

3. 4Dorsch,R. G.,Serafini, J.S.,and Fletcher,E. A. "A Preliminary Investigation of Static-Pressure Changes Associated with Combustion of AluminumBorohydridein a SupersonicWind Tunnel,"NACA RM E55F07,1955.

4. 5Weber,R.J, andMacKay,J.S."AnAnalysisofRamjet EnginesUsingSupersonic Combustion,"NACATN 4386,Sept.1958. 440 G.Y ANDERSON ETAL.

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