Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles.


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    Title :

    Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles


    Additional title:

    NACA -- Report


    Contributors:
    Love, E.S. (author)

    Published in:

    Publication date :

    1955


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :