This paper presents the results of tests and validations of the γ-Reθ model proposed by Menter et al. (2006, “A Correlation-Based Transition Model Using Local Variables—Part I: Model Formation,” ASME J. Turbomach., 128, pp. 413–422), which was extended by in-house correlations for onset location and transition length. The tests performed were based on experimental data from the flat plate test cases available at the ERCOFTAC database as well as on experimental data from the turbine blade profile investigated at Czestochowa University of Technology. Further on, the model was applied for unsteady calculations of the blade profile test case, where chosen inlet conditions (turbulent intensity and wake parameters) were applied. For the selected case, numerical results were compared not only with the experimental data but also with the results obtained with other transition models. It was shown that the applied model was able to reproduce some essential flow features related to the bypass and wake-induced transition, and the simulations revealed good agreement with the experimental results in terms of localization and extent of wake-induced transition.

1.
Savill
,
M.
, 2002, “
New Strategies in Modelling By-Pass Transition
,”
Closure Strategies for Turbulent Transitional Flows
, B. E. Launder and N. Sandham, eds.,
Cambridge University Press
,
Cambridge, UK
, pp.
493
521
.
2.
Dhawan
,
S.
, and
Narasimha
,
R.
, 1958, “
Some Properties of Boundary Layer During the Transition From Laminar to Turbulent Flow Motion
,”
J. Fluid Mech.
0022-1120,
3
, pp.
418
436
.
3.
Vilmin
,
S.
,
Savill
,
M. A.
,
Hodson
,
H. P.
, and
Dawes
,
W. N.
, 2003, “
Predicting Wake-Passing Transition in Turbomachinery Using an Intermittency-Conditioned Modelling Approach
,”
33rd AIAA Fluid Dynamics Conference and Exhibit
, Orlando, June.
4.
Elsner
,
W.
,
Vilmin
,
S.
,
Drobniak
,
S.
, and
Piotrowski
,
W.
, 2004, “
Experimental Analysis and Prediction of Wake-Induced Transition in Turbomachinery
,” ASME Paper No. GT2004-T53757.
5.
Lardeau
,
S.
, and
Leschziner
,
M.
, 2006, “
Modeling of Wake-Induced Transition in Linear Low-Pressure Turbine Cascades
,”
AIAA J.
,
44
(
8
), pp.
1854
1865
. 0001-1452
6.
Lodefier
,
K.
, and
Dick
,
E.
, 2006, “
Modelling of Unsteady Transition in Low-Pressure Turbine Blade Flows With Two Dynamic Intermittency Equations
,”
Flow, Turbul. Combust.
1386-6184,
76
, pp.
103
132
.
7.
Menter
,
F. R.
,
Langtry
,
R. B.
,
Likki
,
S. R.
,
Suzen
,
Y. B.
,
Huang
,
P. G.
, and
Völker
,
S.
, 2006, “
A Correlation-Based Transition Model Using Local Variables—Part I: Model Formation
,”
ASME J. Turbomach.
0889-504X,
128
, pp.
413
422
.
8.
Lodefier
,
K.
,
Dick
,
E.
,
Piotrowski
,
W.
, and
Elsner
,
W.
, 2007, “
Validation of a Dynamic Intermittency Model for the Prediction of Wake-Induced Transition on Turbine Blades
,”
Proceedings of the Seventh European Turbomachinery Conference
, Athens, pp.
1379
1388
.
9.
Medic
,
G.
, and
Durbin
,
P. A.
, 2002, “
Toward Improved Prediction of Heat Transfer on Turbine Blades
,”
ASME J. Turbomach.
0889-504X,
124
, pp.
187
192
.
10.
Zarzycki
,
R.
, and
Elsner
,
W.
, 2005, “
The Effect of Wake Parameters on the Transitional Boundary Layer on Turbine Blade
,”
Proc. Inst. Mech. Eng., Part A
0957-6509,
219
, pp.
471
480
.
11.
Lodefier
,
K.
,
Dick
,
E.
,
Piotrowski
,
W.
, and
Elsner
,
W.
, 2005, “
Modelling of Wake Induced Transition With Dynamic Description of Intermittency
,”
Proceedings of the Sixth European Turbomachinery Conference
, Lille, pp.
730
739
.
12.
Lardeau
,
S.
, and
Leschziner
,
M.
, 2005, “
Unsteady RANS Modelling of Wake-Blade Interaction: Computational Requirements and Limitations
,”
Comput. Fluids
,
34
, (
1
), pp.
3
21
. 0045-7930
13.
Piotrowski
,
W.
,
Lodefier
,
K.
,
Kubacki
,
S.
,
Elsner
,
W.
, and
Dick
,
E.
, 2008, “
Comparison of Two Unsteady Intermittency Models for Bypass Transition Prediction on a Turbine Blade Profile
,”
Flow, Turbul. Combust.
,
81
, pp.
369
394
. 1386-6184
14.
Mayle
,
R. E.
, 1991, “
The Role of Laminar-Turbulent Transition in Gas Turbine Engines
,”
ASME J. Turbomach.
0889-504X,
113
, pp.
509
537
.
You do not currently have access to this content.