This paper contains a tabulation of functions of the Mach number which are frequently used in high-speed aerodynamics. The tables extend from M = 0 to M = 10.0 in increments of 0.01 and are based on the assumption that air is a perfect gas having a specific heat ratio of 1.400.


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    Titel :

    Compressible Flow Tables for Air


    Beteiligte:

    Erscheinungsdatum :

    01.01.1947


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Burcher, Marie A. | TIBKAT | 1948


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