Inlet starting predictions for sidewall-compression scramjet inlets-Reference-Cited by-同舟云学术

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Inlet starting predictions for sidewall-compression scramjet inlets

Published:1988-07-11 Issue: Volume: Page:
ISSN:
Container-title:24th Joint Propulsion Conference
language:
Short-container-title:

Author:

TREXLER CARL¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-3257

Reference5 articles.

1. Research for the Langley Airframe Integrated Scramjet. 1983 JANNAF Propulsion meeting, CPIA Publication,Vol. V, pp.661-675, February 1984. 5. mexler, C. A.The Design and Performance at

2. Mach 4.0 Of Two-Strut Hypersonic Inlets for an Integrated Scramjet Concept. NASA R(-4022, M Y ,1988. (CONFIDENTIAL) LEngine modules

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5. Analysis of a Three-Dimensional, High Pressure Ratio Scramjet Inlet with Variable Internal Contraction;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

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