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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    Titel :

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


    Beteiligte:
    G. S. Pick (Autor:in) / C. J. Martin (Autor:in)

    Erscheinungsdatum :

    1967


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch