A Correlation-Based Transition Model Using Local Variables—Part I: Model FormulationSource: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 003::page 413DOI: 10.1115/1.2184352Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A new correlation-based transition model has been developed, which is based strictly on local variables. As a result, the transition model is compatible with modern computational fluid dynamics (CFD) approaches, such as unstructured grids and massive parallel execution. The model is based on two transport equations, one for intermittency and one for the transition onset criteria in terms of momentum thickness Reynolds number. The proposed transport equations do not attempt to model the physics of the transition process (unlike, e.g., turbulence models) but form a framework for the implementation of correlation-based models into general-purpose CFD methods. Part I (this part) of this paper gives a detailed description of the mathematical formulation of the model and some of the basic test cases used for model validation, including a two-dimensional turbine blade. Part II (, , , , , and , 2006, ASME J. Turbomach., 128(3), pp. 423–434) of the paper details a significant number of test cases that have been used to validate the transition model for turbomachinery and aerodynamic applications. The authors believe that the current formulation is a significant step forward in engineering transition modeling, as it allows the combination of correlation-based transition models with general purpose CFD codes.
keyword(s): Momentum , Turbulence , Reynolds number , Boundary layers , Equations , Thickness , Flow (Dynamics) , Computational fluid dynamics AND Turbine blades ,
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contributor author | S. R. Likki | |
contributor author | Y. B. Suzen | |
contributor author | P. G. Huang | |
contributor author | S. Völker | |
contributor author | F. R. Menter | |
contributor author | R. B. Langtry | |
date accessioned | 2017-05-09T00:21:55Z | |
date available | 2017-05-09T00:21:55Z | |
date copyright | July, 2006 | |
date issued | 2006 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28730#413_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/134816 | |
description abstract | A new correlation-based transition model has been developed, which is based strictly on local variables. As a result, the transition model is compatible with modern computational fluid dynamics (CFD) approaches, such as unstructured grids and massive parallel execution. The model is based on two transport equations, one for intermittency and one for the transition onset criteria in terms of momentum thickness Reynolds number. The proposed transport equations do not attempt to model the physics of the transition process (unlike, e.g., turbulence models) but form a framework for the implementation of correlation-based models into general-purpose CFD methods. Part I (this part) of this paper gives a detailed description of the mathematical formulation of the model and some of the basic test cases used for model validation, including a two-dimensional turbine blade. Part II (, , , , , and , 2006, ASME J. Turbomach., 128(3), pp. 423–434) of the paper details a significant number of test cases that have been used to validate the transition model for turbomachinery and aerodynamic applications. The authors believe that the current formulation is a significant step forward in engineering transition modeling, as it allows the combination of correlation-based transition models with general purpose CFD codes. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | A Correlation-Based Transition Model Using Local Variables—Part I: Model Formulation | |
type | Journal Paper | |
journal volume | 128 | |
journal issue | 3 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2184352 | |
journal fristpage | 413 | |
journal lastpage | 422 | |
identifier eissn | 1528-8900 | |
keywords | Momentum | |
keywords | Turbulence | |
keywords | Reynolds number | |
keywords | Boundary layers | |
keywords | Equations | |
keywords | Thickness | |
keywords | Flow (Dynamics) | |
keywords | Computational fluid dynamics AND Turbine blades | |
tree | Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 003 | |
contenttype | Fulltext |