Application of Oswatitsch's theorem to supercritical airfoil drag calculation
- 1 May 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 30 (3) , 415-416
- https://doi.org/10.2514/3.46354
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Analysis of Embedded Shock Waves Calculated by Relaxation MethodsAIAA Journal, 1974