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An Integral Solution for Skin Friction in Turbulent Flow Over Aerodynamically Rough Surfaces With an Arbitrary Pressure Gradient
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The combined law of the wall and wake, with the inclusion of the “roughness depression function†for the inner law in the “Log†region, is used as the inner coordinates' velocity profile in the integral form of the ...
Rough Surface Turbulent Boundary Layer Heat Transfer Using Generalized Reynolds Analogies
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Stanton number, St, calculations as a function of position, x, are made for turbulent, external boundary layer flow over aerodynamically rough surfaces and also for a fully developed duct flow with rough top and bottom ...
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