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Compressible turbulent Boundary Layers with combined air injection and pressure gradient

Compressible turbulent Boundary Layers with combined air injection and pressure gradient PDF 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

Compressible turbulent Boundary Layers with combined air injection and pressure gradient PDF Author: G. D. Thomas
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

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).

Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients

Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients PDF Author: Shimer Zane Pinckney
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 68

Book Description

Compressible Turbulent Boundary Layers

Compressible Turbulent Boundary Layers PDF Author:
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 580

Book Description

Reynolds Number and Pressure Gradient Effects on Compressible Turbulent Boundary Layers

Reynolds Number and Pressure Gradient Effects on Compressible Turbulent Boundary Layers PDF Author: M. Acharya
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description

The Compressible Turbulent Boundary Layer with Surface Mass Transfer

The Compressible Turbulent Boundary Layer with Surface Mass Transfer PDF Author: Fred Culick
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 80

Book Description

An Experimental Documentation of Pressure Gradient and Reynolds Number Effects on Compressible Turbulent Boundary Layers

An Experimental Documentation of Pressure Gradient and Reynolds Number Effects on Compressible Turbulent Boundary Layers PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 120

Book Description

Calculation of Compressible Turbulent Boundary Layers with Pressure Gradients and Heat Transfer

Calculation of Compressible Turbulent Boundary Layers with Pressure Gradients and Heat Transfer PDF Author: Larry L. Lynes
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 146

Book Description

An Investigation of the High Speed Turbulent Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient: The Compressibility transformation

An Investigation of the High Speed Turbulent Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient: The Compressibility transformation PDF Author: Constantino Economos
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 52

Book Description
This report investigates the behavior of high speed turbulent boundary layer with heat transfer and streamwise pressure gradient.

Compressible Turbulent Boundary Layers with Heat Transfer and Pressure Gradient in Flow Direction

Compressible Turbulent Boundary Layers with Heat Transfer and Pressure Gradient in Flow Direction PDF Author: Alfred Walz
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 28

Book Description

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