Measurements were made in the variable density wind tunnel to determine the pressure distribution over one section of a R.A.F. 31 airfoil with a leading edge slot fully open. To provide data for the study of scale effect on this type of airfoil, the tests were conducted with air densities of approximately one and twenty atmospheres.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Pressure Distribution on a Slotted R.A.F. 31 Airfoil in the Variable Density Wind Tunnel


    Contributors:

    Publication date :

    1929-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English