Application of Unsteady Airfoil Theory to Rotary Wings

• 1 July 1981
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
• Vol. 18  (7) , 604-605
• https://doi.org/10.2514/3.57534

Abstract

Keywords

• LIFT
• AERODYNAMICS
• AEROELASTICITY
• AIRSPEED
• ANGULAR VELOCITY