Author: L. O. F. JerominPublisher:
ISBN:
Category :
Languages : en
Pages : 62
Book Description
An Experimental Investigation of the Compressible Turbulent Boundary Layer with Air Injection
Author: L. O. F. JerominAn Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient
Author: David L. BrottPublisher:
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).
Experimental Investigation of the Compressible Turbulent Boundary Layer at Very High Reynolds Numbers, M
Author: D. R. MooreAn Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient
Author: David L. BrottPublisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 80
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).
An Experimental Investigation of a Compressible Turbulent Boundary Layer Subjected to a Systematic Variation of Adverse Pressure Gradients
Author: Paul John WaltrupPreliminary Experimental Investigation of Effect of Free-stream Turbulence on Turbulent Boundary-layer Growth
Author: S. J. KlinePublisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 70
Book Description
Further Experimental Investigations of Compressible Turbulent Boundary Layers with Air Injection
Author: Leonard Charles SquirePublisher:
ISBN:
Category : Turbulent boundary layer
Languages : en
Pages : 36
Book Description
An Experimental Investigation of Compressible Turbulent Boundary Layers in an Adverse Pressure Gradient with and Without Surface Curvature
Author: Jung-Hua ChouPublisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 258
Book Description
Author: L. C. Squire
Author: