Measurements of the turbulent near wake of a cone at Mach 6.
- 1 March 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (3), 385-391
- https://doi.org/10.2514/3.3449
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- An Experimental Investigation of Base Flows at Supersonic SpeedsJournal of the Royal Aeronautical Society, 1961