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.
Compressible flow tables for air
Nat Advisory Committee Aeronautics -- Tech Note
1948
33 pages
Report
English
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Compressible Flow Tables for Air
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