An Experimental Investigation Of The Compressible Turbulent Boundary Layer With A Favorable Pressure Gradient
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The paper describes the results of a detailed experimental investigation of a two-dimensional turbulent boundary layer in a favorable pressure gradient where th
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Experimental Investigation of Compressible Boundary Layers Under the Influence of Pressure Gradients
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This study examined the effect of mild pressure gradients on the mean and turbulent flow of high-speed boundary layers. Three Mach numbers (1.7, 3.0 and 5.0) we
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