Results are presented of a wind tunnel investigation conducted at Mach numbers of 0.74 and 1.88 to determine the aerodynamic characteristics of rectangular solid bodies for fineness ratios (FR) of 1, 2, and 3, between 0 and 90 deg angles of attack. All the models had the same frontal area of 1.5 by 1.5 inches. (Author)


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    Title :

    Aerodynamic Characteristics of Rectangular Solid Bodies of Various Fineness Ratios at Mach Numbers of 0.74 and 1.88


    Contributors:
    G. S. Pick (author) / C. J. Martin (author)

    Publication date :

    1967


    Size :

    28 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English