Similarity laws governing relationship between relative profile thickness and free stream Mach number for similar pressure distributions have long been known for plane transonic flow around thin airfoils; these similarity laws are now generalized to be valid for wings of finite aspect ratio.


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    Title :

    Similarity laws for transonic flow around wings of finite aspect ratio


    Additional title:

    Stockholm, Kungl. Tekniska Hogskolan -- Inst Flygteknik (Roy Inst Technology -- Div Aeronautics) TN


    Contributors:


    Publication date :

    1950


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :