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Analysis of Turbulent Flow and Heat Transfer on a Flat Plate at High Mach Numbers with Variable Fluid PropertiesA previous analysis of turbulent heat transfer and flow with variable fluid properties in smooth passages is extended to flow over a flat plate at high Mach numbers, and the results are compared with experimental data. Velocity and temperature distributions are calculated for a boundary layer with appreciative effects of frictional heating and external heat transfer. Viscosity and thermal conductivity are assumed to vary as a power or the temperature, while Prandtl number and specific heat are taken as constant. Skin-friction and heat-transfer coefficients are calculated and compared with the incompressible values. The rate of boundary-layer growth is obtained for various Mach numbers.
Document ID
19980223591
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Report (TR)
Authors
Deissler, R. G.
(NASA Lewis Research Center Cleveland, OH United States)
Loeffler, A. L., Jr.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1959
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TR-R-17
Report Number: NASA-TR-R-17
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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