A RELATIONSHIP BETWEEN LAMINAR AND TURBULENT SKIN-FRICTION IN A CONSTANT PRESSURE BOUNDARY LAYER

A. C. Mandal; J. Dey

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A RELATIONSHIP BETWEEN LAMINAR AND TURBULENT SKIN-FRICTION IN A CONSTANT PRESSURE BOUNDARY LAYER

机译：恒压边界层中层流与湍流皮肤摩擦的关系

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摘要

For constant pressure boundary layers, a simple relationship between the laminar and turbulent skin-frictions has been suggested. At a given Reynolds number, the turbulent skin-friction is found to be ~ (laminar skin-friction)~(0.3) .

机译：对于恒定压力边界层，已经提出了层流和湍流皮肤摩擦之间的简单关系。在给定的雷诺数下，发现湍流的皮肤摩擦为〜（层状皮肤摩擦）〜（0.3）。

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《Journal of the Aeronautical Society of India》 |2009年第4期|519-521|共3页
作者
A. C. Mandal; J. Dey;
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Department of Aerospace Engineering, Indian Institute of Science, Bangalore-560 012, India;

Department of Aerospace Engineering, Indian Institute of Science, Bangalore-560 012, India;

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A RELATIONSHIP BETWEEN LAMINAR AND TURBULENT SKIN-FRICTION IN A CONSTANT PRESSURE BOUNDARY LAYER

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