A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock Wave-Reference-Cited by-同舟云学术

A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock Wave

Published:1973-11 Issue:11 Volume:11 Page:1578-1579
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

KORKEGI R. H.¹

Affiliation:

1. Aerospace Research Laboratories, Wright-Patterson Air Force Base, Ohio

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference3 articles.

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

2. Lowrie, B. W. "Cross-Flows Produced by the Interaction of a Swept Shock Wave with a Turbulent Boundary Layer," Ph.D. thesis,Dec. 1965, Dept. of Engineering,Univ. of Cambridge, Cambridge, England.

3. Shock-wave and boundary-layer phenomena near a flat surface

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