Calculation of the supersonic flow around conical bodies
- 1 January 1973
- journal article
- Published by Elsevier in USSR Computational Mathematics and Mathematical Physics
- Vol. 13 (6) , 228-245
- https://doi.org/10.1016/0041-5553(73)90017-7
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Shock-Capturing, Finite-Difference Approach to Supersonic FlowsJournal of Spacecraft and Rockets, 1971
- Delta wing shock shape at hypersonic speedAIAA Journal, 1971
- The calculation of inviscid hypersonic flow past the lower surface of a delta wingJournal of Fluid Mechanics, 1970
- A method for determining the complete flow field around conical wings at supersonic/ hypersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Vortical singularities in conical flow.AIAA Journal, 1967
- Inviscid flowfield about a pointed cone at an angle of attack.AIAA Journal, 1967