Second Approximation to Supersonic Conical Flows
- 1 June 1950
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 17 (6), 328-334
- https://doi.org/10.2514/8.1644
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- CX. The shock strength in supersonic “conical fields.”Journal of Computers in Education, 1949
- SUPERSONIC FLOW ROUND POINTED BODIES OF REVOLUTIONThe Quarterly Journal of Mechanics and Applied Mathematics, 1949
- SUPERSONIC FLOW PAST A SEMI-INFINTE CONEThe Quarterly Journal of Mechanics and Applied Mathematics, 1949
- SUPERSONIC FLOW PAST SLENDER POINTED BODIES OF REVOLUTION AT YAWThe Quarterly Journal of Mechanics and Applied Mathematics, 1948