Effect of nose bluntness on the hypersonic unsteady aerodynamics of an ablating re-entry body.
- 1 June 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 4 (6) , 811-813
- https://doi.org/10.2514/3.28963
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Effect of spherical roughness on hypersonic boundary-layer transition.AIAA Journal, 1966
- Ablation effects on vehicle dynamics.Journal of Spacecraft and Rockets, 1966
- Influence of ablation on the dynamics of slender re-entry configurationsJournal of Spacecraft and Rockets, 1965