Similarity Analysis for Nonequilibrium Turbulent Boundary Layers*Source: Journal of Fluids Engineering:;2004:;volume( 126 ):;issue: 005::page 827DOI: 10.1115/1.1789527Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In his now classical paper on pressure gradient turbulent boundary layers, Clauser concluded that equilibrium flows were very special flows difficult to achieve experimentally and that few flows were actually in equilibrium [1]. However, using similarity analysis of the Navier–Stokes equations, Castillo and George [2] defined an equilibrium flow as one where the pressure parameter, Λ=[δ/(ρU∞2dδ/dx)](dP∞/dx), was a constant. They further showed that most flows were in equilibrium and the exceptions were nonequilibrium flows where Λ≠constant. Using the equations of motion and similarity analysis, it will be shown that even nonequilibrium flows, as those over airfoils or with sudden changes on the external pressure gradient, are in equilibrium state, but only locally. Moreover, in the case of airfoils where the external pressure gradient changes from favorable to zero then to adverse, three distinctive regions are identified. Each region is given by a constant value of Λθ, and each region remains in equilibrium with Λθ=constant, respectively.
keyword(s): Equilibrium (Physics) , Boundary layers , Boundary layer turbulence , Pressure , Flow (Dynamics) , Nonequilibrium flow , Pressure gradient , Reynolds number , Gradients AND Thickness ,
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contributor author | Luciano Castillo | |
contributor author | Xia Wang | |
date accessioned | 2017-05-09T00:13:20Z | |
date available | 2017-05-09T00:13:20Z | |
date copyright | September, 2004 | |
date issued | 2004 | |
identifier issn | 0098-2202 | |
identifier other | JFEGA4-27201#827_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/130193 | |
description abstract | In his now classical paper on pressure gradient turbulent boundary layers, Clauser concluded that equilibrium flows were very special flows difficult to achieve experimentally and that few flows were actually in equilibrium [1]. However, using similarity analysis of the Navier–Stokes equations, Castillo and George [2] defined an equilibrium flow as one where the pressure parameter, Λ=[δ/(ρU∞2dδ/dx)](dP∞/dx), was a constant. They further showed that most flows were in equilibrium and the exceptions were nonequilibrium flows where Λ≠constant. Using the equations of motion and similarity analysis, it will be shown that even nonequilibrium flows, as those over airfoils or with sudden changes on the external pressure gradient, are in equilibrium state, but only locally. Moreover, in the case of airfoils where the external pressure gradient changes from favorable to zero then to adverse, three distinctive regions are identified. Each region is given by a constant value of Λθ, and each region remains in equilibrium with Λθ=constant, respectively. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Similarity Analysis for Nonequilibrium Turbulent Boundary Layers* | |
type | Journal Paper | |
journal volume | 126 | |
journal issue | 5 | |
journal title | Journal of Fluids Engineering | |
identifier doi | 10.1115/1.1789527 | |
journal fristpage | 827 | |
journal lastpage | 834 | |
identifier eissn | 1528-901X | |
keywords | Equilibrium (Physics) | |
keywords | Boundary layers | |
keywords | Boundary layer turbulence | |
keywords | Pressure | |
keywords | Flow (Dynamics) | |
keywords | Nonequilibrium flow | |
keywords | Pressure gradient | |
keywords | Reynolds number | |
keywords | Gradients AND Thickness | |
tree | Journal of Fluids Engineering:;2004:;volume( 126 ):;issue: 005 | |
contenttype | Fulltext |