The Problem of Obtaining High Lift-Drag Ratios at Supersonic Speeds
- 1 May 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (5), 298-302
- https://doi.org/10.2514/8.8049
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- On Optimum Thin Lifting Surfaces at Supersonic SpeedsJournal of the Aerospace Sciences, 1958
- Reduction of Drag Due to Lift in Supersonic Flight by Distributing Lift Along a FuselageJournal of the Aeronautical Sciences, 1956
- Theoretical Determination of the Minimum Drag of Airfoils at Supersonic SpeedsJournal of the Aeronautical Sciences, 1952
- Aerodynamic Performance of Delta Wings at Supersonic SpeedsJournal of the Aeronautical Sciences, 1947