Conical Shock-Wave Angle
- 1 July 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (7) , 1359-1360
- https://doi.org/10.2514/3.55074
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- INTEGRAL APPROACH TO AN APPROXIMATE ANALYSIS OF THRUST VECTOR CONTROL BY SECONDARY INJECTIONAIAA Journal, 1963
- APPROXIMATIONS FOR SUPERSONIC FLOW OVER CONESAIAA Journal, 1963