Experimental study of airfoil performance with vortex generators

Publisher Website

1 May 1987

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

Vol. 24 (5) , 305-309
https://doi.org/10.2514/3.45445

Abstract

No abstract available

This publication has 1 reference indexed in Scilit:

INTRODUCTION TO SHOCK-INDUCED SEPARATION AND ITS PREVENTION BY DESIGN AND BOUNDARY LAYER CONTROL
Published by Elsevier ,1961