Supercritical airfoil drag reduction by passive shock wave/boundary layer control in the Mach number range .75 to .90

Publisher Website

14 January 1985

proceedings article
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.1985-207

Abstract

No abstract available

This publication has 2 references indexed in Scilit:

Unleashing the Hotel Sales Tigers
Cornell Hospitality Quarterly, 1984
Passive shock wave/boundary layer control for transonic airfoil dragreduction
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1983