Numerical Comparison Between Exact and Approximate Theories of Hypersonic Inviscid Flow Past Slender Blunt Nosed Bodies
- 1 May 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
- Vol. 30 (5), 463-468
- https://doi.org/10.2514/8.5120
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Theoretical Pressure Distribution on a Hemisphere-Cylinder CombinationJournal of the Aerospace Sciences, 1959
- Inviscid Hypersonic Flow Over Blunt-Nosed Slender BodiesJournal of the Aeronautical Sciences, 1957
- Dynamics of a dissociating gas Part I Equilibrium flowJournal of Fluid Mechanics, 1957
- On the Propagation and Structure of a Blast Wave, IIJournal of the Physics Society Japan, 1954
- Cylindrical Shock Waves Produced by Instantaneous Energy ReleaseJournal of Applied Physics, 1954
- On the Propagation and Structure of the Blast Wave, IJournal of the Physics Society Japan, 1953