Paper presents results of parametric design studies on application of laminar-flow-control; it is shown that optimum LFC airplane will have lower wing loading than conventional airplane designed for same purposes; comparing optimized high-payload turbulent and LFC configurations, range improvements on order of 20% to 25% can be achieved; configurations for long-range medium payload requirements show even greater range improvements.


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    Titel :

    LFC on large logistics aircraft


    Weitere Titelangaben:

    Astronautics Aeronautics


    Beteiligte:
    Chuprun, J. (Autor:in) / Cahill, J.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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