Pressures measured on upper and lower surface at one chord section on both main airfoil and on flap for several different flap deflections and at several angles of attack; test installation was used in which airfoil was mounted horizontally in wind tunnel between vertical end planes so that two-dimensional flow was approximated. (10¢)


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    Titel :

    Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:


    Erscheinungsdatum :

    1938


    Format / Umfang :

    15 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :