Investigation conducted in Langley Memorial Aeronautical Laboratory 7 by 10-ft wind tunnel to determine air loads on airfoil in combination with fixed leading edge slot and slotted flap; pressures were measured over upper and lower surfaces of component parts of combination for several angles of attack and at several flap settings; data presented as pressure diagrams.


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    Title :

    Pressure distribution over NACA 23012 airfoil with fixed slot and slotted flap


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Harris, T.A. (author) / Lowry, J.G. (author)


    Publication date :

    1942


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




    Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap

    Wenzinger, C.J. / Delano, J.B. | Engineering Index Backfile | 1938


    Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap

    Wenzinger, C.J. / Delano, J.B. | Engineering Index Backfile | 1938


    Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap

    Purser, P.E. / Fischel, J. / Riebe, J.M. | Engineering Index Backfile | 1943