Author: G. D. Thomas
Publisher:
ISBN: 9780114709242
Category : Boundary layer
Languages : en
Pages : 75
Book Description
Compressible turbulent Boundary Layers with combined air injection and pressure gradient
Author: G. D. Thomas
Publisher:
ISBN: 9780114709242
Category : Boundary layer
Languages : en
Pages : 75
Book Description
Publisher:
ISBN: 9780114709242
Category : Boundary layer
Languages : en
Pages : 75
Book Description
An Experimental Investigation of the Compressible Turbulent Boundary Layer with a Favorable Pressure Gradient
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).
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).
Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients
Author: Shimer Zane Pinckney
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 68
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 68
Book Description
Compressible Turbulent Boundary Layers
The Compressible Turbulent Boundary Layer with Surface Mass Transfer
Author: Fred Culick
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 80
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 80
Book Description
Calculation of Compressible Turbulent Boundary Layers with Pressure Gradients and Heat Transfer
Author: Larry L. Lynes
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 146
Book Description
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 146
Book Description
Reynolds Number and Pressure Gradient Effects on Compressible Turbulent Boundary Layers
Turbulent Boundary Layers in Compressible Gases
Author: Samson Semenovich Kutateladze
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 200
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 200
Book Description
An Experimental Documentation of Pressure Gradient and Reynolds Number Effects on Compressible Turbulent Boundary Layers
Analysis of Turbulent Boundary Layers
Author: Tuncer Cebeci
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 430
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 430
Book Description