Shock/boundary-layer interaction control with vortex generators and passive cavity

Author:

Publisher website

1 January 1993

journal article
Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal

Vol. 31 (1) , 91-96
DOI:10.2514/3.11323

Abstract

No abstract available

Keywords

BOUNDARY LAYER

This publication has 5 references indexed in Scilit:

Numerical analysis of shock-induced separation alleviation using vortex generators
1992
Turbulent flow separation control through passive techniques
1989
Interactions between shock waves and turbulent boundary layers
Progress in Aerospace Sciences, 1970
Mixing length and kinematic eddy viscosity in a compressible boundary layer.
AIAA Journal, 1968
INTRODUCTION TO SHOCK-INDUCED SEPARATION AND ITS PREVENTION BY DESIGN AND BOUNDARY LAYER CONTROL
1961