Laminar heat transfer to spherically blunted cones at hypersonic conditions
- 1 March 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (3), 438-444
- https://doi.org/10.2514/3.2349
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- AERODYNAMIC TESTING AT MACH NUMBERS FROM 15 TO 20Published by Elsevier ,1962
- Hypersonic Flow with Combined Leading-Edge Bluntness and Boundary-Layer Displacement EffectPublished by Defense Technical Information Center (DTIC) ,1960
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- Flow with a detached shock wave about a symmetrical profileJournal of Applied Mathematics and Mechanics, 1958
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- Theory of Stagnation Point Heat Transfer in Dissociated AirJournal of the Aerospace Sciences, 1958
- Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight SpeedsJournal of Jet Propulsion, 1956