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Tables of Mach number from 0 to 100 for compressible gases with specific heat ratios from 1.66 through 1.10Mach numbers from 0 to 100 for compressible gases with specific heat ratios 1.66 to 1.10 - table
Document ID
19660028124
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dembrow, D. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-55567
X-470-66-269
Report Number: NASA-TM-X-55567
Report Number: X-470-66-269
Accession Number
66N37414
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TABLE
SPECIFIC HEAT
MACH NUMBER
COMPRESSIBLE FLUID

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