On Curved Shocks in Steady Plane Flow of an Ideal Fluid
- 1 December 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (12) , 826-828
- https://doi.org/10.2514/8.2495
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of AttackJournal of the Aeronautical Sciences, 1952
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951
- On Curved Shock WavesJournal of Mathematics and Physics, 1947