Test results of a fixed geometry RBCC inlet-Reference-Cited by-同舟云学术

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Test results of a fixed geometry RBCC inlet

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Goldman A.¹,Willis B.²

Affiliation:

1. Boeing Rocketdyne Propulsion and Power, Canoga Park, CA

2. NASA, GRC Plum Brook Station, Sandusky, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2589

Reference10 articles.

1. Trexler, C. A. "Inlet Starting Predictions For Sidewall-Compression Scramjet Inlets0022, A&4-88-3257, 24'h Joint Propulsion Conference, July 1988

2. Trexler, C. A. " Inlet Performance Of The Integrated Langlet Scramjet Module0022, AIAA 75-1212, AIAAISEA 1lib Propulsion Conference, Sept 1975

3. Anderson, M. R., and Ortwerth, P. J. "Report On The Inlet Marching Code0022, Rocketdyne NASP-91-047, June 1991

4. 99-2589

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1. Start Limits and Positive Control of RBCC Inlet;Journal of Aerospace Engineering;2022-03

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