NASA NTRS · 20050019404
Compressible Flow Tables for Air
Abstract
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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Burcher, Marie A.. 1947-01-01. Compressible Flow Tables for Air. https://ntrs.nasa.gov/citations/20050019404
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