Physical model of the swept shock wave/boundary-layer interaction flowfield-Reference-Cited by-同舟云学术

Physical model of the swept shock wave/boundary-layer interaction flowfield

Published:1992-09 Issue:9 Volume:30 Page:2252-2258
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Alvi F. S.¹,Settles G. S.¹

Affiliation:

1. Pennsylvania State University, University Park, Pennsylvania 16802

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.11212

Reference25 articles.

1. Swept shock/boundary-layer interactions - Tutorial and update

2. Skin-friction measurements and computational comparison of swept shock/boundary-layer interactions

3. 4Lu, F. K. "Fin-Generated Shock-Wave Boundary-Layer Interactions," Ph.D. Dissertation, Mechanical Engineering Dept., Pennsylvania State Univ.University Park, PA,1988.

4. 5Oskam, B. "Three-Dimensional Flowfields Generated by the Interaction of a Swept Shock Wave with a Turbulent Boundary Layer," Ph.D. Dissertation, Aerospace and Mechanical Sciences Dept.Princeton Univ., Princeton, NJ,Sept. 1976.

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