Turbulent Heat Transfer Through a Highly Cooled, Partially Dissociated Boundary Layer
- 1 December 1958
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 25 (12) , 751-760
- https://doi.org/10.2514/8.7880
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Development of the Calorimeter Heat Transfer Gauge for Use in Shock TubesReview of Scientific Instruments, 1958
- Theory of Stagnation Point Heat Transfer in Dissociated AirJournal of the Aerospace Sciences, 1958
- Experimental Investigation of Turbulent Boundary Layers in Hypersonic FlowJournal of the Aeronautical Sciences, 1955