The flowfield structure of the 3-D shock wave - Boundary layer interaction generated by a 20 deg sharp fin at Mach 3-Reference-Cited by-同舟云学术

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The flowfield structure of the 3-D shock wave - Boundary layer interaction generated by a 20 deg sharp fin at Mach 3

Published:1986-01-06 Issue: Volume: Page:
ISSN:
Container-title:24th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

KNIGHT D.¹,HORSTMAN C.²,BOGDONOFF S.³

Affiliation:

1. Rutgers University, Piscataway, NJ

2. NASA, Ames Research Center, Moffett Field, CA

3. Princeton University, NJ

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-343

Reference51 articles.

1. Glancing Interaction Between a Shock Wave and a Boundary Layer," British ARC CP-555, July 1960. %cCabe, A. "The Three-Dimensional Interaction

Cited by 20 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Reynolds number effects in swept-shock-wave/turbulent-boundary-layer interaction;AIAA Journal;1995-05

2. Supersonic and hypersonic shock/boundary-layer interaction database;AIAA Journal;1994-07

3. Computation of Navier-Stokes equations for three-dimensional flow separation;AIAA Journal;1991-10

4. An experimental/computational study of heat transfer in sharp fin induced turbulent interactions at Mach 5;22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference;1991-06-24

5. An exploratory study of a three-dimensional shock wave turbulent boundary layer interaction in a corner;29th Aerospace Sciences Meeting;1991-01-07

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