Values tabulated include -- pressure ratio, temperature ratio, area ratio, nondimensional mass flow with respect to total pressure, nondimensional mass flow with respect to static pressure, and velocity divided by square root of total temperature; applicability of tables to various propulsion calculations.


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    Title :

    Compressible gas flow tables for specific heat ratio γ=4/3 (mach number 0.000 to 2.000)


    Additional title:

    Canada. Nat Research Council -- Aeronautical Report


    Contributors:


    Publication date :

    1962


    Size :

    40 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :