Increases in camber resulted in large increases in lift and drag divergence Mach numbers at high values of lift coefficient and in augmentation of maximum lift coefficient.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Effects of amount and type of camber on variation with Mach number of aerodynamic characteristics of 10-percent-thick NACA 64A-series airfoil section


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Summers, J.L. (author) / Treon, S.L. (author)


    Publication date :

    1950


    Size :

    66 pages


    Remarks:

    Charts, tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :