A numerical method for calculating steady unsymmetrical supersonic flow past cones
- 30 June 1970
- journal article
- Published by Elsevier in Journal of Computational Physics
- Vol. 5 (3) , 463-486
- https://doi.org/10.1016/0021-9991(70)90075-6
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
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- Supersonic flow past cones of general cross-sectionJournal of Fluid Mechanics, 1962
- Hypersonic flows past a yawed circular cone and other pointed bodiesJournal of Fluid Mechanics, 1962
- On the Structure of Vortical Layers in Supersonic and Hypersonic FlowsJournal of the Aerospace Sciences, 1960
- Experiments on Circular Cones at Yaw in Supersonic FlowJournal of the Aeronautical Sciences, 1956
- A VORTICAL SINGULARITY IN CONICAL FLOWThe Quarterly Journal of Mechanics and Applied Mathematics, 1954
- On Supersonic Flow Past a Slightly Yawing Cone IIJournal of Mathematics and Physics, 1951
- On Supersonic Flow Past A Slightly Yawing ConeJournal of Mathematics and Physics, 1948