A convenient, explicit formula for oblique- shock calculations.
- 1 September 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 5 (5) , 509-510
- https://doi.org/10.2514/3.43975
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A New Formula for Pressure Versus Flow Deflection at Hypersonic SpeedsJournal of the Royal Aeronautical Society, 1967
- Applications of Hypersonic Small-Disturbance TheoryJournal of the Aeronautical Sciences, 1954