Modeling the response from a cascade to an upstream acoustic disturbance-Reference-Cited by-同舟云学术

Modeling the response from a cascade to an upstream acoustic disturbance

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Paynter Gerald¹,Clark Larry¹,Cole Gary²

Affiliation:

1. Boeing Co., Seattle, WA

2. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-953

Reference17 articles.

1. Hedges, L.,Lewis, 1, Carlin, C.,andBeck, C. "SupersonicInletSimulationwithClosedLoopControland MovingControlSurfaces,"AIAAPaper 96-0493,January 1996.

2. Cole, G.L.,Melcher, K.J.,Chicatelli, A.K.,Hartley, T. T., and Chung, J. K. "Computational Methods for HSCT-Inlet Controls/CFD Interdisciplinary Research,"AIAA Paper 94-3209,June 1994.

3. Prediction of supersonic inlet unstart caused by freestream disturbances

4. Clark,L.T."Dynamic ResponseCharacteristicsofa MixedCompressionSupersonicInletasPartofaLarger System,"AIAAPaper 95-0036,January 1995.

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