Differential Analysis For The Turbulent Boundary Layer On A Compressor Blade Element Including Boundary Layer Separation PDF Download
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Author | : James F. Schmidt |
Publisher | : |
Total Pages | : 36 |
Release | : 1974 |
Genre | : Compressors |
ISBN | : |
Download Differential Analysis for the Turbulent Boundary Layer on a Compressor Blade Element (including Boundary-layer Separation) Book in PDF, ePub and Kindle
A two-dimensional differential analysis is developed to approximate the turbulent boundary layer on a compressor blade element with strong adverse pressure gradients, including the separated region with reverse flow. The predicted turbulent boundary layer thicknesses and velocity profiles are in good agreement with experimental data for a cascade blade, even in the separated region.
Author | : |
Publisher | : |
Total Pages | : 810 |
Release | : 1974 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 500 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : Arnold Polak |
Publisher | : |
Total Pages | : 58 |
Release | : 1971 |
Genre | : Boundary layer control |
ISBN | : |
Download The Prediction of Turbulent Boundary-layer Separation Influenced by Blowing Book in PDF, ePub and Kindle
The report presents an analysis predicting separation of a turbulent boundary layer over a cone-flare configuration with gas injected into the boundary layer ahead of separation point. Separation location and separation lengths are compared with experimental data obtained at Mach number of 6 and a range of Reynolds numbers. At the highest Reynolds numbers the extent of separation decreases with increasing Reynolds number. When compared to separation over cylinder-flare body it is found that the extent of separation is lower for the cone-flare configuration. (Author).
Author | : |
Publisher | : |
Total Pages | : 1570 |
Release | : 1974 |
Genre | : Government publications |
ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 620 |
Release | : 1974 |
Genre | : Mechanics, Applied |
ISBN | : |
Download Applied Mechanics Reviews 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).
Author | : Tuncer Cebeci |
Publisher | : |
Total Pages | : 430 |
Release | : 1974 |
Genre | : Science |
ISBN | : |
Download Analysis of Turbulent Boundary Layers Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1456 |
Release | : 1974 |
Genre | : Technology |
ISBN | : |
Download Government Reports Announcements Book in PDF, ePub and Kindle
Author | : Donald M. Kuehn |
Publisher | : |
Total Pages | : 32 |
Release | : 1961 |
Genre | : Noses (Space vehicles) |
ISBN | : |
Download Turbulent Boundary-layer Separation Induced by Flares on Cylinders at Zero Angle of Attack Book in PDF, ePub and Kindle