Loads induced by terminal-shock boundary-layer interaction on cone-cylinder bodies
- 1 September 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 7 (9) , 1106-1112
- https://doi.org/10.2514/3.30109
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- An application of automatic carpet plotting to wind-tunnel data reduction.Journal of Spacecraft and Rockets, 1967
- Analysis of flow separation effects on the dynamics of a large space boosterJournal of Spacecraft and Rockets, 1965