Calculation Of Turbulent Boundary Layers With Heat Transfer And Pressure Gradient Utilizing A Compressibility Transformation Part 1 Summary Report
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Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation
Author | : J. Boccio |
Publisher | : |
Total Pages | : 50 |
Release | : 1972 |
Genre | : Equations of motion |
ISBN | : |
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of mass transfer and pressure gradient, is presented in this paper. A strip-integral method is employed whereby two of the three governing equations are obtained by integrating the combined momentum and continuity equation to 50 percent and 100 percent, respectively, of the boundary-layer height. The latter equation is the usual momentum-integral equation; the former equation requires specification of shear. Accordingly, Clauser's equilibrium eddy-viscosity law is assumed valid at this point. The third and final equation is obtained by specifying that Stevenson's velocity profiles apply throughout the domain of interest, from which a skin-friction law can be derived. Comparisons of the numerical results with the experiments of McQuaid, which include combined effects of variable pressure gradient and mass transfer, show good agreement.
Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation
Author | : C. Economos |
Publisher | : |
Total Pages | : |
Release | : 1971 |
Genre | : Differential equations, Partial |
ISBN | : |
An Investigation of the High Speed Turbulent Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient: The Compressibility transformation
Author | : Constantino Economos |
Publisher | : |
Total Pages | : 52 |
Release | : 1970 |
Genre | : Heat |
ISBN | : |
This report investigates the behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradient.