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Compressible Flow Tables for AirThis 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.
Document ID
20050019404
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Burcher, Marie A. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 22, 2013
Publication Date
January 1, 1947
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-RM-L7K26
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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