An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient PDF Download

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An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient

An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient PDF Author: David L. Brott
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 104

Book Description
The paper describes the results of a detailed experimental investigation of a two-dimensional turbulent boundary layer in a favorable pressure gradient where the free-stream Mach number varied from 3.8 to 4.6 and the ratio of wall to adiabatic-wall temperature has a nominal value of 0.82. Detailed profile measurements were made with pressure and temperature probes; skin friction was measured directly with a shear balance. The velocity- and temperature-profile results were compared with zero pressure gradient and incompressible results. The skin-friction data were correlated with momentum-thickness Reynolds number and pressure-gradient parameter. (Author).
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