A Method Of Calculation Compressible Turbulent Boundary Layers
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Author | : H. James Herring |
Publisher | : |
Total Pages | : 99 |
Release | : 1968 |
Genre | : |
ISBN | : |
Download A Method of Calculation Compressible Turbulent Boundary Layers Book in PDF, Epub and Kindle
Author | : H. James Herring |
Publisher | : |
Total Pages | : 124 |
Release | : 1968 |
Genre | : Turbulent boundary layer |
ISBN | : |
Download A Method of Calculating Compressible Turbulent Boundary Layers Book in PDF, Epub and Kindle
Author | : Dennis M. Bushnell |
Publisher | : |
Total Pages | : 156 |
Release | : 1977 |
Genre | : Compressibility |
ISBN | : |
Download Calculation Methods for Compressible Turbulent Boundary Layers, 1976 Book in PDF, Epub and Kindle
Author | : Shimer Zane Pinckney |
Publisher | : |
Total Pages | : 68 |
Release | : 1971 |
Genre | : Boundary layer |
ISBN | : |
Download Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients Book in PDF, Epub and Kindle
Author | : Neal Tetervin |
Publisher | : |
Total Pages | : 96 |
Release | : 1967 |
Genre | : Enthalpy |
ISBN | : |
Download An Approximate Method for the Calculation of the Reynolds Analogy Factor for a Compressible Turbulent Boundary Layer in a Pressure Gradient Book in PDF, Epub and Kindle
The method predicts that a positive pressure gradient increases and a negative pressure gradient decreases the ratio of Stanton number to friction coefficient. The Crocco relation between the velocity and total enthalpy for a non-adiabatic surface and zero pressure gradient is generalized to non-zero pressure gradient. The relation between the velocity and the total enthalpy varies markedly from the flat plate Crocco relation as the pressure gradient departs from zero. The magnitude of the variation depends on the velocity profile shape parameter. (Author).
Author | : Dennis M. Bushnell |
Publisher | : |
Total Pages | : 156 |
Release | : 1977 |
Genre | : Turbulent boundary layer |
ISBN | : |
Download Calculation Methods for Compressible Turbulent Boundary Layers--1976 Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 580 |
Release | : 1969 |
Genre | : Compressibility |
ISBN | : |
Download Compressible Turbulent Boundary Layers Book in PDF, Epub and Kindle
Author | : Tuncer Cebeci |
Publisher | : Elsevier |
Total Pages | : 423 |
Release | : 2012-12-02 |
Genre | : Technology & Engineering |
ISBN | : 0323151051 |
Download Analysis of Turbulent Boundary Layers Book in PDF, Epub and Kindle
Analysis of Turbulent Boundary Layers focuses on turbulent flows meeting the requirements for the boundary-layer or thin-shear-layer approximations. Its approach is devising relatively fundamental, and often subtle, empirical engineering correlations, which are then introduced into various forms of describing equations for final solution. After introducing the topic on turbulence, the book examines the conservation equations for compressible turbulent flows, boundary-layer equations, and general behavior of turbulent boundary layers. The latter chapters describe the CS method for calculating two-dimensional and axisymmetric laminar and turbulent boundary layers. This book will be useful to readers who have advanced knowledge in fluid mechanics, especially to engineers who study the important problems of design.
Author | : Larry L. Lynes |
Publisher | : |
Total Pages | : 146 |
Release | : 1969 |
Genre | : Air flow |
ISBN | : |
Download Calculation of Compressible Turbulent Boundary Layers with Pressure Gradients and Heat Transfer Book in PDF, Epub and Kindle
Author | : M. C. Altstatt |
Publisher | : |
Total Pages | : 46 |
Release | : 1976 |
Genre | : Compressibility |
ISBN | : |
Download Evaluation of a Method for Computation of Separated, Turbulent, Compressible Boundary Layers Book in PDF, Epub and Kindle
A computer code for a turbulent, compressible boundary-layer method, capable of carrying out computations in a region of separated flow, is developed and tested. The procedure after separation is to specify either friction velocity or boundary-layer thickness as an independent variable and obtain external velocity as a dependent variable. This requires a trial and error alternation of the specified variable in order to match the desired experimental or computed external velocity. Satisfactorily results were obtained by this method in the analysis of certain specialized cases of separated flow. (Author).