Alleviation of Spin-Entry Tendencies through Localization of Wing-Flow Separation
Open Access
- 1 February 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (2) , 69-75
- https://doi.org/10.2514/3.57467
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Exploratory study of the influence of wing leading-edge modifications on the spin characteristics of a low-wing single-engine general aviation airplanePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Historical Overview of Stall/Spin Characteristics of General Aviation AircraftJournal of Aircraft, 1979
- A method for localizing wing flow separation at stall to alleviate spin entry tendenciesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978