It is shown that wing stall can be encountered even though entire wing is immersed in propeller slipstream; effects of wing stall on power requirements in transition speed range and on take off and landing distance; with stall under control, STOL performance becomes primarily function of amount of power installed in airplane.


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    Titel :

    Take-off and landing distance and power requirements of propeller-driven STOL airplanes


    Weitere Titelangaben:

    Aeronautical Eng Rev


    Beteiligte:
    Kuhn, R.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Ducted propeller for STOL airplanes

    Raspet, A. | Engineering Index Backfile | 1960


    Problems in design of propeller-driven vertical take-off transport airplanes

    McKinney, M.O. / Kuhn, R.E. / Hammack, J.B. | Engineering Index Backfile | 1956



    Introduction to V/STOL airplanes

    Kohlman, D. L. | TIBKAT | 1981