NASA Technical Note
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Page : 434 pages
File Size : 22,37 MB
Release : 1972
Category :
ISBN :
Author :
Publisher :
Page : 434 pages
File Size : 22,37 MB
Release : 1972
Category :
ISBN :
Author : Tuncer Cebeci
Publisher : Elsevier
Page : 423 pages
File Size : 31,19 MB
Release : 2012-12-02
Category : Technology & Engineering
ISBN : 0323151051
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.
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Page : 1730 pages
File Size : 21,47 MB
Release : 1970
Category : Government publications
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Page : 744 pages
File Size : 28,55 MB
Release : 1987
Category : Astronautics
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Author : United States. Superintendent of Documents
Publisher :
Page : 1348 pages
File Size : 19,26 MB
Release : 1970
Category : United States
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Author : United States. Superintendent of Documents
Publisher :
Page : 1320 pages
File Size : 30,74 MB
Release : 1966
Category : Government publications
ISBN :
Author :
Publisher :
Page : 316 pages
File Size : 10,40 MB
Release : 1992
Category : Aeronautics
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Author :
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Page : 580 pages
File Size : 43,14 MB
Release : 1971
Category : Aeronautics
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Author : Daniel W. Lester
Publisher :
Page : 562 pages
File Size : 32,40 MB
Release : 1979
Category : Government publications
ISBN :
Author : Earl R. Keener
Publisher :
Page : 60 pages
File Size : 26,7 MB
Release : 1972
Category : Aerodynamics, Hypersonic
ISBN :
Velocity profiles were obtained from pitot-pressure and total-temperature measurements within a turbulent boundary layer on a large sharp-edged flat plate. Momentum-thickness Reynolds number ranged from 2590 to 8860 and wall-to-adiabatic-wall temperature ratios ranged from 0.3 to 0.5. Measurements were made both with and without boundary layer trips. Five methods are evaluated for correlating the measured velocity profiles with the incompressible law-of-the-wall and the velocity defect law. The mixing-length generalization of Van Driest gives the best correlation.