Influence of Asymmetric Transition on Re-Entry Vehicle Characteristics
- 1 May 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (5) , 476-482
- https://doi.org/10.2514/3.59681
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Effect of boundary-layer transition on vehicle dynamicsJournal of Spacecraft and Rockets, 1969
- Shock tunnel investigation of boundary-layer transition at M equals 5.5.AIAA Journal, 1967
- Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight SpeedsJournal of Jet Propulsion, 1956