To determine effect of acceleration on development of lift in simulated carrier-deck catapult takeoff for 2-dimensional wing, unswept wing, swept and delta planform wing; each of wings developed 90% of its steady-state lift within 7 chord lengths of travel; results agreed qualitatively with those calculated from theory.


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    Titel :

    Wind-tunnel investigation of development of lift on wings in accelerated longitudinal motion


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Turner, T.R. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :