Applying slender wing benefits to military aircraft
- 1 August 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (8) , 545-559
- https://doi.org/10.2514/3.45023
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Application of Free Vortex Sheet theory to slender wings with leading-edge vortex flapsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Aerodynamic Features of Designed Strake-Wing ConfigurationsJournal of Aircraft, 1982
- The unsteady suction analogy and applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Effects of Spanwise Blowing on Two Fighter Airplane ConfigurationsJournal of Aircraft, 1980
- Evolution of the hybrid wing - YF-17/F-18 typePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Development of a vortex-lift-design method and application to a slender maneuver-wing configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980