Investigation of Local Laminar Heat Transfer on a Hemisphere for Supersonic Mach Numbers at Low Rates of Heat Flux
- 1 March 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (3), 188-194
- https://doi.org/10.2514/8.3801
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A Note on Soviet ScienceThe Russian Review, 1957
- Calculation Method for Three-Dimensional Rotationally Symmetrical Laminar Boundary Layers with Arbitrary Free-Stream Velocity and Arbitrary Wall-Temperature VariationJournal of the Aeronautical Sciences, 1953
- EQUIPMENT AND TECHNIQUES FOR MAKING PRESSURE MEASUREMENTS IN SUPERSONIC WIND TUNNELS AT MACH NUMBERS UP TO 5Published by Defense Technical Information Center (DTIC) ,1952
- LXXXV.Solutions of the boundary-layer equationsJournal of Computers in Education, 1931