Analysis of flow separation effects on the dynamics of a large space booster
- 1 July 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 2 (4) , 481-490
- https://doi.org/10.2514/3.28216
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- A MECHANISM FOR SELF-EXCITED OSCILLATIONS OF “HAMMERHEAD” AND OTHER BLUNT-NOSE MISSILESPublished by Elsevier ,1961