Model with unswept wing and high disk loading fan mounted in fuselage duct was tested in wind tunnel; results were used to study transition flight characteristics associated with submerged fan concept; fan produced large pitching moment variation with increasing forward speed; programming required use of wing flaps, variable angle of attack, and direct propulsive thrust.


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    Titel :

    Aerodynamics of fan-in-fuselage model


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Maki, R.L. (Autor:in) / Hickey, D.H. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamics of fuselage

    Multhopp, H. | Engineering Index Backfile | 1942


    Aerodynamics of the fuselage

    Multhopp, H. | TIBKAT | 1942


    Aerodynamics of the Fuselage

    Multhopp, H. | NTRS | 1942


    Aerodynamics of the Fuselage

    H. Multhopp | NTIS | 1942


    AERODYNAMICS OF A FAN-IN-FUSELAGE MODEL

    Hickey, D. H. / Maki, R. L. | NTRS | 1960