A Semiempirical Method for Determining Delta-Wing Pressure Distributions in an Incompressible Flow
- 1 December 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (12) , 854-856
- https://doi.org/10.2514/8.3244
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Slender-Body Theory-Review and ExtensionJournal of the Aeronautical Sciences, 1953
- The Lift Distribution on Low Aspect Ratio Wings at Subsonic SpeedsJournal of the Aeronautical Sciences, 1951