Tabulation of functions of Mach number which are frequently used in high speed aerodynamics; tables include values of Mach number from 0 to 10.0 in increments of 0.01 and functions are based on assumption that air is perfect gas having specific-heat ratio of 1.400.


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    Title :

    Compressible flow tables for air


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Compressible Flow Tables for Air

    Burcher, Marie A. | NTRS | 1947


    Compressible flow tables for air

    Burcher, Marie A. | TIBKAT | 1948


    Compressible flow tables for air

    Burcher, Marie A | NTRS | 1948