The Turbulent Boundary Layer On A Cylinder In Axial Flow PDF Download

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Turbulent Boundary Layer on a Cylinder in Axial Flow

Turbulent Boundary Layer on a Cylinder in Axial Flow
Author:
Publisher:
Total Pages: 66
Release: 1988
Genre:
ISBN:

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This report reviews research on the turbulent boundary layer that develops on a cylinder in axial flow. Experimental results indicate that the transverse curvature results in a higher coefficient of friction and a fuller velocity profile than for a planar boundary layer. However, appropriate scaling laws and nondimensional scaling parameters are still elusive. The few turbulence measurements such as Reynolds stress and intermittency that are available for a cylindrical boundary layer suggest that the distribution of turbulent quantities in the boundary layer is somewhat different from a planar boundary layer, particularly as the boundary layer becomes thick compared to the radius of the cylinder. This is most likely a result of the tendency for a cylindrical boundary layer to become wake-like as the cylinder becomes very small. Measurements of turbulence intensity and detection of turbulence-generating events in a cylindrical boundary layer suggest that the mechanism for the production of turbulence near the wall is similar to that for other wall-bounded flows. However, there is experimental evidence that the outer flow interacts with the near-wall flow to modify the generation of turbulence. Suggestions for further work include more comprehensive and sophisticated measurements of turbulent quantities in cylindrical boundary layers as well as computational modeling.


Turbulent Boundary-layer and Skin-friction Measurements in Axial Flow Along Cylinders at Mach Numbers Between 0.5 and 3.6

Turbulent Boundary-layer and Skin-friction Measurements in Axial Flow Along Cylinders at Mach Numbers Between 0.5 and 3.6
Author: Dean R. Chapman
Publisher:
Total Pages: 53
Release: 1954
Genre: Turbulent boundary layer
ISBN:

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Experiments have been conducted to determine average skin-friction coefficients in the absence of heat transfer for competely turbulent flow along the cylindrical portion of cone-cylinder bodies of revolution having over-all fineness ratios of 10, 15, and 25. The friction data were obtained by directly measuring forces. Numerous boundary-layer surveys were made to enable all data to be based on an effective starting postion of the turbulent flow. Mach numbers of 0.5. 0.8, 2.0, 2.5, 2.9, 3.4, and 3.6, and Reynolds numbers between 4 million and 32 million were investigated. At a Mach number of 2.0, data were obtained for different pressure distributions by distorting the flexible-plate walls of the wind tunnel.


The Axisymmetric Turbulent Boundary Layer on an Extremely Long Cylinder

The Axisymmetric Turbulent Boundary Layer on an Extremely Long Cylinder
Author: Frank M. White
Publisher:
Total Pages: 26
Release: 1969
Genre:
ISBN:

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An analysis is presented which predicts the properties of an arbitrarily thick turbulent boundary layer in axial flow past a long cylinder. The study makes use of a modified form of the turbulent law-of-the-wall, which properly accounts for transverse curvature effects. Using this law, the theory which follows is then an exact solution to the axisymmetric equations of continuity and momentum in incompressible flow. Numerical results are given to show the effect of curvature on the various boundary layer characteristics. Skin friction and drag coefficients can be increased greatly with increasing curvature while boundary layer thickness is decreased. When defined in their axisymmetric form, the displacement and momentum thickness are both decreased by curvature. The velocity profile is flattened greatly and the shape factor approaches unity at large curvature. The failure of earlier power-law theories to make accurate predictions is shown to be due to their inadequate handling of the strong profile shape changes. (Author).