Experimental Investigation of Flow Around Lifting Symmetrical Double-Wedge Airfoils at Mach Numbers of 1.30 and 1.41.


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    Title :

    Experimental investigation of flow around lifting symmetrical double-wedge airfoils at mach numbers of 1.30 and 1.41


    Additional title:

    NACA -- Tech Note


    Contributors:
    Gooderum, P.B. (author) / Wood, G.P. (author)


    Publication date :

    1956


    Size :

    86 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :