Contents: Predicted and measured performance of two full-scale ducted propellers; Aerothermal dynamic performance of a high bypass tip turbine cruise fan system; Thrust deflection nozzles for VTOL aircraft; Shrouded propeller research at Mississippi State University leading to application on the United States Army XV-11A; The lift, drag and stability of wings immersed in propeller slipstream; Aerodynamic properties of airfoils in nonuniformly sheared flows; Experimental investigation of compound helicopter aerodynamic interference effects; Maximum lift coefficient for STOL aircraft: a critical review.


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    Titel :

    Cal/Usaavlabs Symposium Proceedings. Aerodynamic Problems Associated with V/STOL Aircraft. Volume II. Propulsion and Interference Aerodynamics. Held June 23, 1966, Statler-Hilton Hotel, Buffalo, New York


    Erscheinungsdatum :

    1966


    Format / Umfang :

    330 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch