Measurements made in variable-density wind tunnel to determine pressure distribution over one section of R.A.F.-31 airfoil with leading edge slot fully open, to provide data for study of scale effect; tests conducted with air densities of approximately 1 and 20 atmospheres; full-scale maximum lift somewhat lower than maximum lift indicated by low scale.


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    Title :

    Pressure distribution on a slotted R.A.F. 31 airfoil in the variable density wind tunnel


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Notes


    Contributors:


    Publication date :

    1929


    Size :

    13 pages


    Remarks:

    12 Figs., Supp. plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :