Numerical Study on Supersonic Inlet Buzz Under Various Throttling Conditions and Fluid-Structure Interaction-Reference-Cited by-同舟云学术

Numerical Study on Supersonic Inlet Buzz Under Various Throttling Conditions and Fluid-Structure Interaction

Published:2011-06-27 Issue: Volume: Page:
ISSN:
Container-title:29th AIAA Applied Aerodynamics Conference
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Author:

Hong Wooram¹,Kim Chongam¹

Affiliation:

1. Seoul National University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3967

Reference20 articles.

1. Oswatitsch, K. "Pressure Recovery in Missiles with Reaction Propulsion at High Supersonic Speeds (the Efficiency of ShockDiffusers),"NACATM-1140, 1947.

2. Supersonic Diffuser Instability

3. Ferri, A., andNucci, R.M. "TheOrigin ofAerodynamicInstabilityofSupersonicInlets atSubcritical Conditions,"NACA RM-L50K30, Jan.1951.

4. Numerical Simulation of Near-Critical and Unsteady, Subcritical Inlet Flow

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