Minimum Drag Cambered Rectangular Wing for Supersonic Speeds
- 1 September 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (9) , 642-643
- https://doi.org/10.2514/8.2770
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- A Drag Reduction Method for Wings of Fixed Plan FormJournal of the Aeronautical Sciences, 1952