Calculation of Flow-Variable Gradients Behind Curved Shock Waves
- 1 December 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (12) , 958-959
- https://doi.org/10.2514/8.8826
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- The Rolling Up of the Trailing Vortex Sheet and Its Effect on the Downwash Behind WingsJournal of the Aeronautical Sciences, 1951
- Calculation of Curvatures of Attached Shock WavesJournal of Mathematics and Physics, 1948