One-Dimensional Scanning Approach to Shock Sensing-Reference-Cited by-同舟云学术

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One-Dimensional Scanning Approach to Shock Sensing

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Tokars Roger¹,Adamovsky Grigory¹,Floyd Bertram²

Affiliation:

1. NASA Glenn Research Center

2. Sierra Lobo/NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1454

Reference34 articles.

1. Wilcox,F.A. and Perchonok,E. "Aerodynamic ControlofHypersonicInletsforOptimum Performance," NACA Research Memorandum,NACARME55L1,1956.

2. Cattafesta, L.N., IIIand Settles, G.S."Experiments on Shock/VortexInteraction", AIAA-92-0315

3. Hewett,M.D."High-SpeedCivilTransportIssuesandTechnologyProgram,"NASA CR-186020,1992.

4. Ray, J.K,Carlin, C.M.,andLambregts, "High-Speed CivilTransportFlight-Propulsion-Control TechnologicalIssues,"NASACR-186015,1992.

5. 5Saiben, M, Donovan, J, F., and Morris, M.J. "FlightPrototypeNormal ShockSensor,"NASA CR-18520, 1990.

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