Contents: A theory for static propeller performance; Propeller testing at zero velocity; Propeller research at Canadair Limited; Prediction of the performance and stress characteristics of VTOL propellers; Performance potential of rotor blade inboard aerodynamic devices; Aerodynamic loading of high-speed rotors; Prediction of rotor wake flows; The movement, structure and breakdown of trailing vortices from a rotor blade.
Cal/Usaavlabs Symposium Proceedings. Aerodynamic Problems Associated with V/STOL Aircraft. Volume I. Propeller and Rotor Aerodynamics. Held June 22, 1966, Statler-Hilton Hotel, Buffalo, New York
1966
275 pages
Report
Keine Angabe
Englisch
Aircraft , Fluid Mechanics , Aerodynamics , Helicopters , Aerodynamic characteristics , Vertical take-off planes , Short take-off planes , Symposia , Propellers(Aerial) , Rotor blades(Rotary wings) , Performance(Engineering) , Helicopter rotors , Tests , Stresses , Predictions , Aerodynamic loading , Wake , Vortices , Theory