Modified thin shock layer method for supersonic flow past an oscillating cone
- 1 August 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 13 (8) , 481-487
- https://doi.org/10.2514/3.27920
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
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- Elements of GasdynamicsPhysics Today, 1957
- Newtonian Flow Theory for Slender BodiesJournal of the Aeronautical Sciences, 1957
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- The air pressure on a cone moving at high speeds.—IProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1933