Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effects of Mach Number Up to 0.34 and Reynolds Number Up to 8 x 10(exp 6) on the Maximum Lift Coefficient of a Wing of NACA 66-Series Airfoil Sections


    Contributors:

    Publication date :

    1950


    Size :

    46 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English