Computational-experimental pressure distributions on a transonic, low-aspect-ratio wing
- 17 August 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Experimental and Computational Investigation of a Swept-Wing Flow at Subsonic SpeedsJournal of Aircraft, 1979