An experimental investigation of the shock layer surrounding a sphere in supersonic flow
- 1 March 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (3), 451-457
- https://doi.org/10.2514/3.2885
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- A CRITICAL STUDY OF THE DIRECT BLUNT BODY INTEGRAL METHODPublished by Defense Technical Information Center (DTIC) ,1962
- PRESSURE DISTRIBUTIONS ON A HEMISPHERE CYLINDER AT SUPERSONIC AND HYPERSONIC MACH NUMBERSPublished by Defense Technical Information Center (DTIC) ,1961
- An Experimental Investigation of Blunt Body Stagnation Point Velocity GradientARS Journal, 1959