Surface phenomena in a three-dimensional skewed shock wave/laminar boundary-layer interaction-Reference-Cited by-同舟云学术

Surface phenomena in a three-dimensional skewed shock wave/laminar boundary-layer interaction

Published:1984-12 Issue:12 Volume:22 Page:1764-1769
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Degrez G.¹,Ginoux J. J.²

Affiliation:

1. Universite Libre de Bruxelle, Brussels, Belgium

2. Karman Institute for Fluid Dynamics, Rhode Saint Genese, Belgium

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.8849

Reference29 articles.

1. 3Lowrie, B. W. "Cross Flow Produced by the Interaction of a Swept Shock Wave with a Turbulent Boundary Layer," Ph.D. Thesis,University of Cambridge, Cambridge, England, Dec. 1965.

2. The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary Layer

3. Supersonic interference flow along the corner of intersecting wedges.

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