An Investigation of Laminar, Transitional, and Turbulent Heat Transfer on Blunt-Nosed Bodies in Hypersonic Flow
- 1 June 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (6), 401-414
- https://doi.org/10.2514/8.8571
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Turbulent Heat Transfer Through a Highly Cooled, Partially Dissociated Boundary LayerJournal of the Aerospace Sciences, 1958
- Measurement of Turbulent Heat Transfer Rates on the Aft Portion and Blunt Base of a Hemisphere Cylinder in the Shock TubeJournal of Jet Propulsion, 1958
- Transformation of the Compressible Turbulent Boundary LayerJournal of the Aerospace Sciences, 1958
- A PROCEDURE FOR CALCULATING THE BOUNDARY-LAYER DEVELOPMENT IN THE REGION OF TRANSITION FROM LAMINAR TO TURBULENT FLOWPublished by Defense Technical Information Center (DTIC) ,1957