Some Features of Supersonic and Hypersonic Flow About Blunted Cones
- 1 April 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (4) , 389-399
- https://doi.org/10.2514/8.9473
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
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- An Approximate Solution of the Direct Supersonic Blunt-Body Problem for Arbitrary Axisymmetric ShapesJournal of the Aerospace Sciences, 1960
- Theoretical Pressure Distribution on a Hemisphere-Cylinder CombinationJournal of the Aerospace Sciences, 1959
- The Supersonic Blunt-Body Problem - Review and ExtensionJournal of the Aerospace Sciences, 1958
- Inviscid Hypersonic Flow Over Blunt-Nosed Slender BodiesJournal of the Aeronautical Sciences, 1957
- Readers ForumJournal of the Aeronautical Sciences, 1956
- The Generalized Shock-Expansion Method and Its Application to Bodies Traveling at High Supersonic Air SpeedsJournal of the Aeronautical Sciences, 1955
- Interferometric Studies of Supersonic Flows about Truncated ConesJournal of Applied Physics, 1953