Boundary-Layer Transition and Heat Transfer in Shock Tubes
- 1 August 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (8), 587-594
- https://doi.org/10.2514/8.8656
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- The Effect of Extreme Cooling and Local Conditions on Boundary-Layer TransitionJournal of the Aerospace Sciences, 1958
- Experiments on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- Measurement of Wall Temperature and Heat Flow in the Shock TubeJournal of Applied Physics, 1955