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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    Title :

    Aerodynamics of fan-in-fuselage model


    Additional title:

    NASA -- Tech Note


    Contributors:
    Maki, R.L. (author) / Hickey, D.H. (author)


    Publication date :

    1961


    Size :

    14 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Aerodynamics of fuselage

    Multhopp, H. | Engineering Index Backfile | 1942


    Aerodynamics of the fuselage

    Multhopp, H. | TIBKAT | 1942


    Aerodynamics of the Fuselage

    H. Multhopp | NTIS | 1942


    Aerodynamics of the Fuselage

    Multhopp, H. | NTRS | 1942


    AERODYNAMICS OF A FAN-IN-FUSELAGE MODEL

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