Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation. Part 2: Constant Property Turbulent Boundary Layer Flow with Simultaneous Mass Transfer and Pressure Gradient
Title | Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation. Part 2: Constant Property Turbulent Boundary Layer Flow with Simultaneous Mass Transfer and Pressure Gradient PDF eBook |
Author | |
Publisher | |
Pages | 52 |
Release | 1972 |
Genre | |
ISBN |
Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation. Part 3: Computer Program Manual
Title | Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation. Part 3: Computer Program Manual PDF eBook |
Author | |
Publisher | |
Pages | 110 |
Release | 1972 |
Genre | |
ISBN |
Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation
Title | Calculation of Turbulent Boundary Layers with Heat Transfer and Pressure Gradient Utilizing a Compressibility Transformation PDF eBook |
Author | J. Boccio |
Publisher | |
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.
Scientific and Technical Aerospace Reports
Title | Scientific and Technical Aerospace Reports PDF eBook |
Author | |
Publisher | |
Pages | 1572 |
Release | 1992 |
Genre | Aeronautics |
ISBN |
Monthly Catalog of United States Government Publications
Title | Monthly Catalog of United States Government Publications PDF eBook |
Author | |
Publisher | |
Pages | 1932 |
Release | 1972 |
Genre | Government publications |
ISBN |
The Aeronautical Journal
Title | The Aeronautical Journal PDF eBook |
Author | |
Publisher | |
Pages | 672 |
Release | 1972 |
Genre | Aeronautics |
ISBN |
Monthly Catalog of United States Government Publications, Cumulative Index
Title | Monthly Catalog of United States Government Publications, Cumulative Index PDF eBook |
Author | United States. Superintendent of Documents |
Publisher | |
Pages | 1466 |
Release | 1976 |
Genre | United States |
ISBN |