Test description and preliminary pitot-pressure surveys for Langley Test Technique Demonstrator at Mach 6-Reference-Cited by-同舟云学术

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Test description and preliminary pitot-pressure surveys for Langley Test Technique Demonstrator at Mach 6

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

EVERHART JOEL¹,ASHBY, JR. GEORGE¹,MONTA WILLIAM¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3940

Reference24 articles.

1. Cubbage,James, M.; and, Mercer,CharlesE. "lnvestigatbn of EffeUof PropulsionSystem lnstallatbnandOpeFatbnOnAerodynamicsofan AiWathingHypersonicAilphneatMach 0.3to 1.2". NASATND-8503,July 1977.

2. Cubbage,JamesM.; andMom,WilllamJ. "Surface PressureDataonaScramjetExternalNozzle ModelatMach 6UdngaSimlanlGasfortheEngine ExhaustFbw." NASPContractorReport 1058,August 1989.

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