Computing Transient Gas Flows with Shock Waves
- 1 October 1964
- journal article
- research article
- Published by AIP Publishing in Physics of Fluids
- Vol. 7 (10) , 1713-1715
- https://doi.org/10.1063/1.1711078
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Direct Calculation of Pressure Distribution on Blunt Hypersonic Nose Shapes With Sharp CornersJournal of the Aerospace Sciences, 1961
- An Approximate Solution of the Direct Supersonic Blunt-Body Problem for Arbitrary Axisymmetric ShapesJournal of the Aerospace Sciences, 1960
- A Method for the Numerical Calculation of Hydrodynamic ShocksJournal of Applied Physics, 1950