Inlet Flow Control Technology: Learning from History, Reinventing the Future-Reference-Cited by-同舟云学术

Inlet Flow Control Technology: Learning from History, Reinventing the Future

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Surber Lewis¹,Tinapple Jon²

Affiliation:

1. Universal Technology Corporation

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-12

Reference9 articles.

1. Oswatitisch,Kl,"PressureRecoveryfor MissileswithReactionPropulsionatHigh SupersonicSpeeds(The EfficiencyofShock Diffusers), NACAT.M. 1140,Jun1947 (Translated froma1944 GermanDocument.)

2. Surber,Syberg,"Performanceof Highly Integrated InletsforSupersonicAircraft," AerodynamicsofPower Plant Installation, AGARDCP-301,Toulouse,France,May1981.

3. Wind Tunnel and Flight Performance of the YF-12 Inlet System

4. Cuttrell,Tinapple,"LongRangeStrike Aircraft Air-BreathingPropulsion Integration,"CAF 33615-00-3053, D.O. 0021, AFRL/RBAIFinal Report,24April 2003.

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