Three-dimensional shock wave turbulent boundary layer interaction for a 20 deg sharp fin at Mach 3-Reference-Cited by-同舟云学术

Three-dimensional shock wave turbulent boundary layer interaction for a 20 deg sharp fin at Mach 3

Published:1987-03-24 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

BOGDONOFF S.¹,SHAPEY B.²

Affiliation:

1. Princeton University, NJ

2. Rockwell International Corp., Rocketdyne Div., Canoga Park, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-554

Reference9 articles.

1. Oakem, B. "Three-Dimensional Flow Fields Generated by the Interaction of a Swept Shock Wave with a Turbulent Boundary Layer." Ph.D. Thesis,Mechanical and Aerospace Engineering Department, Princeton University, September 1976.

2. Knight, D., Horstman,C., Shapey. B., and Bogdonoff, S. "The Flowfield Structure of the 3-0 Shock Wave/Boundary Layer Interaction Generated by a 200 Sharp Fin et Mach 3," AIM 86-0343,1986.

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