Streamline curvature and velocity gradient behind curved shocks.
- 1 September 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (9) , 1352-1354
- https://doi.org/10.2514/3.6926
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Calculation of Flow-Variable Gradients Behind Curved Shock WavesJournal of the Aerospace Sciences, 1960