An investigation of separated flow about a hemisphere-cylinder at incidence in the Mach number range from 0.6 to 1.5

Publisher Website

24 January 1977

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

https://doi.org/10.2514/6.1977-179

Abstract

No abstract available

This publication has 1 reference indexed in Scilit:

Separation Patterns of Boundary Layer over an Inclined Body of Revolution
AIAA Journal, 1972