Reduction of Stall-Spin Entry Tendencies Through Wing Aerodynamic Design
- 1 February 1976
- proceedings article
- Published by SAE International
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Design of Low-Speed Airfoils by Numerical OptimizationSAE International Journal of Advances and Current Practices in Mobility, 1975
- Unsteady aerodynamic and stall effects on helicopter rotor blade airfoil sectionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968