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Heat Transmission in the Boundary LayerIn the present paper which deals with the heat transfer between the gas and the wall for large temperature drops and large velocities use is made of the method of Dorodnitsyn of the introduction of a new independent variable, with this difference, however, that the relation between the temperature field (that is, density) and the velocity field in the general case considered is not assumed given but is determined from the solution of the problem. The effect of the compressibility arising from the heat transfer is thus taken into account (at the same time as the effect of the compressibility at the large velocities). A method is given for determining the coefficients of heat transfer and the friction coefficients required in many technical problems for a curved wall in a gas flow at large Mach numbers and temperature drops. The method proposed is applicable both for Prandtl number P = 1 and for P not equal to 1.
Document ID
20050028447
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Kalikhman, L. E.
Date Acquired
August 22, 2013
Publication Date
April 1, 1949
Publication Information
Publication: Prikladnaya Matematika I Mekhanika, Tom X
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-TM-1229
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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