Experimental Effect of Bluntness and Gas Rarefaction on Drag Coefficients and Stagnation Heat Transfer on Axisymmetric Shapes in Hypersonic Flow
- 1 December 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (12), 1429-1432
- https://doi.org/10.2514/8.9861
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Wind tunnel measurements of sphere drag at supersonic speeds and low Reynolds numbersJournal of Fluid Mechanics, 1961