Computation of induced drag for elliptical and crescent-shaped wings
- 1 July 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 30 (4) , 446-452
- https://doi.org/10.2514/3.46365
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Induced drag of wings with highly swept and tapered wing tipsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Minimum induced drag for wings with spanwise camberJournal of Aircraft, 1990
- Reductions in induced drag by the use of aft swept wing tipsThe Aeronautical Journal, 1989
- Convergence of lift and drag predictions by a Morino panel method (VSAERO)AIAA Journal, 1989
- Induced-drag characteristics of crescent-moon-shaped wingsJournal of Aircraft, 1987
- A General Approach to Multiple Lifting Surface Design and AnalysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Prediction of Subsonic Aerodynamic Characteristics: A Case for Low-Order Panel MethodsJournal of Aircraft, 1982
- PAN AIR - A higher order panel method for predicting subsonic or supersonic linear potential flows about arbitrary configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981