Experimental studies on the lip shock.
- 1 February 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (2) , 212-219
- https://doi.org/10.2514/3.4480
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- On the separation of a supersonic flow at a sharp corner.AIAA Journal, 1967
- Effect of a shoulder modification on turbulent supersonic base flow.AIAA Journal, 1967
- Base pressure of slender bodies in laminar, hypersonic flow.AIAA Journal, 1966
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966
- Estimation of the strength of lip shock.AIAA Journal, 1966
- Near wake of a blunt body at hypersonic speedsAIAA Journal, 1965
- An Investigation of Two-Dimensional Supersonic Base PressuresJournal of the Aerospace Sciences, 1958