Modern Adaptation of Prandtl's Classic Lifting-Line Theory
- 1 July 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 37 (4) , 662-670
- https://doi.org/10.2514/2.2649
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Lifting-Line Theory for Arbitrarily Shaped WingsJournal of Aircraft, 1999
- Unsteady low-speed aerodynamic model for complete aircraft configurationsJournal of Aircraft, 1988
- Numerical lifting line theory applied to drooped leading-edge wings below and above stallJournal of Aircraft, 1980
- The oblique wing as a lifting-line problem in transonic flowJournal of Fluid Mechanics, 1980