Numerical Investigation of a Super-Sonic Inlet Using Bleed and Micro-Ramps to Control Shock-Wave/Boundary Layer Interactions-Reference-Cited by-同舟云学术

Numerical Investigation of a Super-Sonic Inlet Using Bleed and Micro-Ramps to Control Shock-Wave/Boundary Layer Interactions

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Atkinson Michael¹

Affiliation:

1. Air Force Research Laboratory/VAAC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-24

Reference12 articles.

1. Rizzetta,D.P. "NumericalSimulationofaSupersonicInlet,"AIAAPaper 91-0128,Jan. 2001.

2. Benson, T.J.,Chyu, W.J., Rimlinger, M.J., Shih, T.I-P.,Willis,B.P. "StructureofShock-Wave/Boundary-Layer Interactions withBleed thoughRowsof Circular Holes,"AIAAPaper 97-0508, Jan.1997.

3. Bodner,J.P., Davis, D.O., Greber, I.,Hingst, W.R. "ExperimentalInvestigationoftheEffectofaSingle Bleed HoleonaSupersonicTurbulentBoundary-Layer,"AIAAPaper 96-2797, July. 1996.

4. Hamed, A., Shang, J.S. "Surveyand AssessmentofValidationDataBasefor ShockWave BoundaryLayer InteractionsinSupersonicInlets,"AIAAPaper 89-2939,July. 1989.

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