Reduction of Drag Due to Lift in Supersonic Flight by Distributing Lift Along a Fuselage
- 1 November 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (11) , 1037-1043
- https://doi.org/10.2514/8.3718
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Handbook of Elliptic Integrals for Engineers and PhysicistsPublished by Springer Nature ,1954
- Theoretical Determination of the Minimum Drag of Airfoils at Supersonic SpeedsJournal of the Aeronautical Sciences, 1952