Effects of sweep and angle of attack on boundary-layer transition on wings at mach number 4.04.


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    Title :

    Effects of sweep and angle of attack on boundary-layer transition on wings at mach number 4.04


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1955


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :