Boundary layer transition flight test observations

Publisher Website

24 January 1977

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

https://doi.org/10.2514/6.1977-125

Abstract

No abstract available

This publication has 2 references indexed in Scilit:

Supersonic boundary-layer transition - Effects of roughness and freestream disturbances
AIAA Journal, 1971
Shock tunnel investigation of boundary-layer transition at M equals 5.5.
AIAA Journal, 1967