Fuel Distribution Depending on Internal Flow Separation in a Scramjet Engine-Reference-Cited by-同舟云学术

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Fuel Distribution Depending on Internal Flow Separation in a Scramjet Engine

Published:2020-03-10 Issue: Volume: Page:
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Container-title:23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Sato Shigeru¹,Fukui Masaaki²,Watanabe Takahiro³,Takahashi Masaharu³,Munakata Toshihiko³

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

2. Space Service

3. Hitachi Global

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

1. 1Curran,E.T.,andMurthy,S.N.B.,Editors,"ScramjetPropulsion,"ProgressinAstronauticsandAeronautics,Vol.189,AIAA2001.

2. 2Auslender,A.H., Suder,K.L., and Thomas,S.R. "An Overview of the NASA FAP Hypersonics Project Airbreathing Propulsion Research,"AIAAPaper2009-7277,2009.

3. 3Falempin,F.,andSerre,L."FrenchFlightTestingProgramLEAStatusin2009,"AIAAPaper2009-7227,2009.

4. 4Razzaqi,S.,Silvester,T.,Smart,M.andPaull,R."TheHIFiRE7FlightExperiment,"AIAAPaper2018-5256,2018.

5. 5Sato,S.,Izumikawa.,M.,Tomioka,S.,andMitani,T."ScramjetEngineTestatMach6FlightCondition,"AIAAPaper97-3021,1997.

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