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Heat Diffusion in Gases, Including Effects of Chemical ReactionThe diffusion of heat through gases is treated where the coefficients of thermal conductivity and diffusivity are functions of temperature. The diffusivity is taken proportional to the integral of thermal conductivity, where the gas is ideal, and is considered constant over the temperature interval in which a chemical reaction occurs. The heat diffusion equation is then solved numerically for a semi-infinite gas medium with constant initial and boundary conditions. These solutions are in a dimensionless form applicable to gases in general, and they are used, along with measured shock velocity and heat flux through a shock reflecting surface, to evaluate the integral of thermal conductivity for air up to 5000 degrees Kelvin. This integral has the properties of a heat flux potential and replaces temperature as the dependent variable for problems of heat diffusion in media with variable coefficients. Examples are given in which the heat flux at the stagnation region of blunt hypersonic bodies is expressed in terms of this potential.
Document ID
20160000713
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Hansen, C. Frederick
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
January 13, 2016
Publication Date
October 1, 1960
Publication Information
Publication: ARS Journal
Volume: 30
Issue: 10
Subject Category
Inorganic, Organic And Physical Chemistry
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: American Rocket Society (ARS) Semi-Annual Meeting
Location: San Diego, CA
Country: United States
Start Date: June 8, 1959
End Date: June 11, 1959
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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