An Experimental Study of Surface Pressure Fluctuations in a Separating Turbulent Boundary Layer

An Experimental Study of Surface Pressure Fluctuations in a Separating Turbulent Boundary Layer PDF Author:
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ISBN:
Category :
Languages : en
Pages : 88

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An Experimental Study of Surface Pressure Fluctuations in a Separating Turbulent Boundary Layer

An Experimental Study of Surface Pressure Fluctuations in a Separating Turbulent Boundary Layer PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 88

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An Experimental Investigation of Surface Pressure Fluctuations Beneath Two and Three-dimensional Turbulent Boundary Layers

An Experimental Investigation of Surface Pressure Fluctuations Beneath Two and Three-dimensional Turbulent Boundary Layers PDF Author: Michael C. Goody
Publisher:
ISBN:
Category :
Languages : en
Pages :

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An Experimental Investigation of Pressure Fluctuations in Three-Dimensional Turbulent Boundary Layers

An Experimental Investigation of Pressure Fluctuations in Three-Dimensional Turbulent Boundary Layers PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Experimental surface pressure fluctuations measurements over a wide range of Reynolds number (1400

Some Features of Surface Pressure Fluctuations in Turbulent Boundary Layers with Zero and Favorable Pressure Gradients

Some Features of Surface Pressure Fluctuations in Turbulent Boundary Layers with Zero and Favorable Pressure Gradients PDF Author: Brian E. McGrath
Publisher:
ISBN:
Category : Boundary layer noise
Languages : en
Pages : 138

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An Experimental Investigation of the Influence of an Air Bubble Layer on Radiated Noise and Surface Pressure Fluctuations in a Turbulent Boundary Layer

An Experimental Investigation of the Influence of an Air Bubble Layer on Radiated Noise and Surface Pressure Fluctuations in a Turbulent Boundary Layer PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

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An experimental investigation is described which shows relationships between the noise spectra of a layer of air bubbles in a turbulent flow and a maximum stable bubble size which can exist in the same flow. An air bubble layer with individual bubble sizes greater than a maximum stable size was introduced into the boundary layer of water flowing along a smooth flat plate. It was found that the maximum stable bubble size was related to the turbulent kinetic energy dissipation as had been previously shown by other investigators for a variety of turbulent flows. A unique 'corner frequency' of the noise spectra which resulted from the bubble splitting down to a maximum stable size could be also related to the turbulent kinetic energy dissipation of the boundary layer flow. (Author).

Annual Research Briefs ...

Annual Research Briefs ... PDF Author: Center for Turbulence Research (U.S.)
Publisher:
ISBN:
Category : Turbulence
Languages : en
Pages : 410

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Experimental Study of a Three-dimensional Shear-driven Turbulent Boundary Layer with Streamwise Adverse Pressure Gradient

Experimental Study of a Three-dimensional Shear-driven Turbulent Boundary Layer with Streamwise Adverse Pressure Gradient PDF Author: David Michael Driver
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 268

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The Separating Turbulent Boundary Layer

The Separating Turbulent Boundary Layer PDF Author: James Hassler Strickland
Publisher:
ISBN:
Category : Boundary layer control
Languages : en
Pages : 430

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Aerodynamics

Aerodynamics PDF Author: Virgil A. Sandborn
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 35

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An experimental study of techniques for modifying the surface shear stress, both mean and fluctuating, in turbulent boundary layers is reported. The surface shear along the test section of a 45.7cm square wind tunnel, with a downstream expansion section, was determined by means of surface-hot-wire-heat-transfer-gauges. Turbulent boundary layers in both zero and adverse pressure gradients were evaluated. The mean and fluctuating surface shear in a zero pressure gradient can be effectively reduced by employing a set of closely spaced fins. The fins protruded from the surface up through the sublayer. The fins produced an effective momentum defect for the boundary layer near the surface, which reduced the surface shear fluctuations by as much as 75 percent, two boundary layer thicknesses downstream, and 52 percent 15 boundary layer thicknesses downstream (the limit of the present experiment). The mean surface shear was also reduced by 35 to 25 percent for the same 2 to 15 boundary thicknesses downstream. The fins do not appear to produce a large increase in the thickness of the layer. No small size device, which could be mounted in the sublayer, was found that could develope a persistent increase in either the mean or fluctuating surface shear. Small scale vortex generators had no measureable effect on the flow for downstream distances greater than approximately 4 to 5 boundary layer thicknesses. Only the large scale vortex generator, normally use to delay boundary layer separation, produced an increase in surface shear at large distances downstream. (Author).

Adverse Pressure Gradient and Separating Turbulent Boundary-layer Flow: the Effect of Disequilibrium in Initial Conditions

Adverse Pressure Gradient and Separating Turbulent Boundary-layer Flow: the Effect of Disequilibrium in Initial Conditions PDF Author: A. D. Cutler (Johnston, J. P.)
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Book Description
This report documents an experimental study of detaching and reattaching boundary layers and boundary layers downstream of a reattachment. Three low Mach number, fully turbulent boundary layers flowing on a flat surface have been.