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.


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    Titel :

    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


    Erscheinungsdatum :

    1966


    Format / Umfang :

    275 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch