Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery 2000
DOI: 10.1115/2000-gt-0520
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Numerical Performance of Transition Models in Different Turbomachinery Flow Conditions: A Comparative Study

Abstract: A numerical study has been performed to compare the overall performance of three transition models when used with an industrial Navier-Stokes solver. The three models investigated include two experimental correlations and an integrated eN method. Twelve test cases in realistic turbomachinery flow conditions have been calculated. The study reveals that all the three models can work numerically well with an industrial Navier-Stokes code, but the prediction accuracy of the models depends on flow conditions. In ge… Show more

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“…In the past, algebraic turbulence models (the Baldwin-Lomax [3][4][5][6] or the Mitchel one [7]), one-equation models (the Spalart-Allmaras one [5; 7]) and two-equation (k − or k − ! ones, see References [6][7][8]) have been used for the analysis of the same problem.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…In the past, algebraic turbulence models (the Baldwin-Lomax [3][4][5][6] or the Mitchel one [7]), one-equation models (the Spalart-Allmaras one [5; 7]) and two-equation (k − or k − ! ones, see References [6][7][8]) have been used for the analysis of the same problem.…”
Section: Introductionmentioning
confidence: 99%
“…ones, see References [6][7][8]) have been used for the analysis of the same problem. In some of these works, criteria for the prediction of the onset of transition based on integral boundary layer quantities (the Abu-Ghannam and Shaw [9] or the Mayle model [1], which are both used in this work) or the integration of the growth rates of instability waves (the so-called e N model [4]) have been used. A few works in which the onset of transition was deÿned by the user can also be found (for instance Reference [5], using the SA model).…”
Section: Introductionmentioning
confidence: 99%