Supersonic flow past circular cones at large angles of attack
- 1 January 1975
- journal article
- Published by Springer Nature in Fluid Dynamics
- Vol. 8 (6), 915-919
- https://doi.org/10.1007/bf01014266
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- A systematic development of the supersonic flow fields over and behind wings and wing-body configurations using a shock-capturing finite-difference approachPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Application of the straight-line method to the calculation of flow past conical bodies at large angles of attackFluid Dynamics, 1967
- Wings in hypersonic flowJournal of Applied Mathematics and Mechanics, 1965
- The calculation of the interaction of non-stationary shock waves and obstaclesUSSR Computational Mathematics and Mathematical Physics, 1962