Measurement of Turbulent Heat Transfer Rates on the Aft Portion and Blunt Base of a Hemisphere Cylinder in the Shock Tube
- 1 September 1958
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Jet Propulsion
- Vol. 28 (9) , 615-620
- https://doi.org/10.2514/8.7405
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight SpeedsJournal of Jet Propulsion, 1956