Basic data consisting of contours of control location for maximum section lift coefficient and for minimum profile drag coefficient for various control deflections also presented.


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    Titel :

    Wind-tunnel investigation of drooped ailerons on 16-percent-thick low-drag airfoil


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Holtzclaw, R.W. (Autor:in) / Dods, Jr., J.B. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    25 pages


    Anmerkungen:

    44 Supp Sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch






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