Aerodynamic characteristics of tilt-wing and deflected slip-stream configurations are examined; it appears that for propeller driven VTO L aircraft, combination of 2 principles (tilt-wing and flap configuration) should be used.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic characteristics of propeller-driven VTOL aircraft


    Additional title:

    NASA -- Tech Note


    Contributors:
    Kirby, R.H. (author)


    Publication date :

    1961


    Size :

    16 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :





    Field requirements of overloaded propeller-driven VTOL aircraft

    Neal, B. / Lyster, H.N.C. | Engineering Index Backfile | 1963


    Design considerations for propeller-driven VTOL

    Robinson, Jr., D.W. | Engineering Index Backfile | 1959