Hot wire measurements of freestream and shock layer disturbances.

Publisher Website

1 December 1971

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

Vol. 9 (12) , 2468-2470
https://doi.org/10.2514/3.6537

Abstract

No abstract available

This publication has 2 references indexed in Scilit:

Nonaffine similarity laws inherent in Newtonian impact theory
AIAA Journal, 1970
Influence of measured freestream disturbances on hypersonic boundary-layer transition
AIAA Journal, 1970