Rear stagnation point location in a subsonic near-wake
- 1 May 1976
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 13 (5) , 319-320
- https://doi.org/10.2514/3.27911
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Experimental Wake Flow Properties of a Viking '75 Entry VehicleJournal of Spacecraft and Rockets, 1974