Thrust hypothesis, concept and experimental verification; "characteristics" for jet-flapped wings at zero and nonzero angle of attack are presented; any combination of jet flap parameters, lift, drag, jet deflection angle, angle of attack, slot blowing rates and engine thrust, efficiency of lift, economic operating ranges, etc, may be read from characteristics; range of most economical jet flap operation coincides with that portion of characteristics over which any increment in jet flap momentum causes exactly same increment in propulsive thrust; application of jet flap principle to STOL aircraft design.


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    Titel :

    Jet flap characteristics for high-aspect-ratio wings


    Weitere Titelangaben:

    AIAA J


    Beteiligte:

    Erschienen in:

    AIAA Journal ; 2 , n 1


    Erscheinungsdatum :

    1964


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :