Development of a Vortex-Lift Design Procedure and Application to a Slender Maneuver-Wing Configuration
- 1 April 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (4) , 259-266
- https://doi.org/10.2514/3.57490
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Analysis and Design of Strake-Wing ConfigurationsJournal of Aircraft, 1980
- Design study results of a supersonic cruise fighter wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Subsonic Vortex-Flow Design Study for Slender WingsJournal of Aircraft, 1978
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971