The report presents the key results of a model wing tunnel test program that was directed towards investigating the use of cyclic pitch propellers as the low speed longitudinal control system of a four propeller V/STOL tilt wing transport-type aircraft. The almost linear pitch control effectiveness of this system through transitional flight and in-ground effect along with the correlation with theory is discussed, and the moderate power increase associated with its use is shown. (Author)


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    Titel :

    Cyclic Pitch Control on a V/STOL Tilt Wing Aircraft


    Beteiligte:
    C. E. Kolesar (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    114 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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