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Approximations for the Thermodynamic and Transport Properties of High-Temperature AirThe thermodynamic and transport properties of high-temperature air are found in closed form starting from approximate partition functions for the major components in air and neglecting all minor components. The compressibility, enthalpy, entropy, the specific heats, the speed of sound, the coefficients of viscosity and of thermal conductivity, and the Prandtl numbers for air are tabulated from 500 degrees to 15,000 degrees Kelvin over a range of pressure from 0.0001 to 100 atmospheres. The energy of air and the mol. fractions of the major components of air can be found from the tabulated values for compressibility and enthalpy. It is predicted that the Prandtl number for fully ionized air, which is in complete equilibrium, will become small compared to unity, the order of 0.01, and this implies that boundary layers in such flow will be very transparent to heat flux.
Document ID
19980237039
Acquisition Source
Ames Research Center
Document Type
Other - NASA Technical Report (TR)
Authors
Hansen, C. Frederick
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
August 18, 2013
Publication Date
January 1, 1959
Subject Category
Fluid Mechanics And Thermodynamics
Aerodynamics
Report/Patent Number
NASA-TR-R-50
Report Number: NASA-TR-R-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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