Heat Mass Transfer And Friction In Turbulent Boundary Layer With List Of References
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Heat-mass Transfer and Friction in a Turbulent Boundary Layer
Author | : Samson Semenovič Kutateladze |
Publisher | : |
Total Pages | : 276 |
Release | : 1974 |
Genre | : |
ISBN | : |
Heat Transfer, Mass Transfer, and Friction in Turbulent Boundary Layers
Author | : Samson Semenovich Kutateladze |
Publisher | : Core/Mechanical |
Total Pages | : 328 |
Release | : 1990 |
Genre | : Science |
ISBN | : |
Reflects the growing practical applications for methods of computing the turbulent boundary layer based on relative limiting friction and heat exchange laws. Highlighted are conditions existing under two-phase flow and novel applications of injection critical parameters.
Analogy Between Mass and Heat Transfer with Turbulent Flow
Author | : Edmund E. Callaghan |
Publisher | : |
Total Pages | : 724 |
Release | : 1953 |
Genre | : Heat |
ISBN | : |
An analysis of combined heat and mass transfer from a flat plate has been made in terms of Prandtl's simpified physical concept of the turbulent boundary layer. The results of the analysis show that tor conditioins of reasonably small heat and mass transfer, the ratio of the mass- and heat-transfer coefficients is dependent on the Reynolds number of the boundary layer, the Prandtl number of the medium of diffusion, and the Schmidt number of the diffusing fluid in the medium of diffusion. For the particular case of water evaporating into air, the ratio of mass-transfer coefficient to heat-transfer coefficient is found to be slightly greater than unity.
Heat-mass Transfer and Friction in a Turbulent Boundary Layer
Author | : Samson Semenovič Kutateladze (Physiker, Russland) |
Publisher | : |
Total Pages | : 276 |
Release | : 1974 |
Genre | : |
ISBN | : |
Heat-mass Transfer and Friction in a Turbulent Boundary Layer
Author | : Samson Semenovich Kutateladze |
Publisher | : |
Total Pages | : 296 |
Release | : 1974 |
Genre | : Mass transfer |
ISBN | : |
A Correlation of Heat-transfer and Skin-friction Data and an Experimental Reynolds Analogy Factor for Highly Cooled Turbulent Boundary Layers at Mach 5.0
Author | : Donald M. Wilson |
Publisher | : |
Total Pages | : 82 |
Release | : 1969 |
Genre | : Heat |
ISBN | : |
Turbulent boundary-layer heat transfer and skin-friction coefficients were measured on sharp slender cones at a free-stream Mach number of 5.0. Wall-to-stagnation temperature ratios from 0.15 to 0.80 were obtained by precooling or preheating the model. Tests were conducted for a wide range of Reynolds numbers by varying the tunnel supply pressure and temperature, thus providing data for naturally turbulent boundary layers. The experimental results were compared with existing theories which predict convective Stanton number or skin-friction coefficients. These comparisons indicate that the heat-transfer data are best predicted by the Spalding-Chi law and the skin friction by the Sommer-Short reference temperature method. The experimental Reynolds analogy factor is adequately predicted by Colburn's incompressible correlation for wall-to-stagnation temperature ratios above about 0.5. However, for lower wall temperature ratios, the experimental Reynolds analogy factor decreases with decreased temperature ratios in a manner which has not been previously reported. (Author).
Analysis of Turbulent Flow and Heat Transfer on a Flat Plate at High Mach Numbers with Variable Fluid Properties
Author | : R. G. Deissler |
Publisher | : |
Total Pages | : 42 |
Release | : 1959 |
Genre | : Aerodynamic heating |
ISBN | : |