Numerical simulation of supersonic flow using a new analytical bleed boundary condition-Reference-Cited by-同舟云学术

Numerical simulation of supersonic flow using a new analytical bleed boundary condition

Published:1995-07-10 Issue: Volume: Page:
ISSN:
Container-title:31st Joint Propulsion Conference and Exhibit
language:
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Author:

Harloff G,Smith G

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-2759

Reference7 articles.

1. Inlet Boundary-Layer-Bleed Flows," AIAA Paper 95-0038,January 1995. 2. Cooper, G.K. and Sirhaugh, J.R. "The PARC

2. proximation and Algebraic Modelfor Separated Turbulent Flows," AIAA paper 78-257, 1978. 4. Baldwin, B.S. and BaIth, T. J. "A One

3. etry Definition/Visual Interactive Rapid Grid Generation, User's Manual," Wright Patterson AFB, January 1990. 6. Willis, B., Davis, D., and Hingst, W. "Flow

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