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¢)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1938


    Size :

    15 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :