A correlation-based transition model using local variables part II - Test cases and industrial applications

Proceedings of the ASME Turbo Expo 2004

Volumn 4, Issue , 2004, Pages 69-79

  Langtry, R B ^a   Menter, F R ^a   Likki, S R ^b   Suzen, Y B ^b   Huang, P G ^b   Volker S ^c  

^a ANSYS INC   (United States)

^b UNIVERSITY OF KENTUCKY   (United States)

^c GENERAL ELECTRIC COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; HEAT TRANSFER; INDUSTRIAL APPLICATIONS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; TURBOMACHINERY;

COMPRESSOR CASCADES; MOMENTUM THICKNESS; TURBULENCE INTENSITY;

COMPUTATIONAL FLUID DYNAMICS;

EID: 10244245023     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-53454     Document Type: Conference Paper

References (13)

1. Mayle, R.E., (1991), "The Role of Laminar-Turbulent Transition in Gas Turbine Engines," ASME Journal of Turbomachinery, Vol. 113, pp. 509-537.
2. Thermann, H., Müller, M., and Niehuis, R., (2001), "Numerical Simulation of the Boundary Layer Transition in Turbomachinery Flows,", ASME paper 2001-GT-0475, New Orleans, 2001.
3. Stieger, R., Hollis, D., and Hodson, H., (2003), "Unsteady Surface Pressures due to Wake Induced Transition in a Laminar Separation Bubble on a LP Turbine Cascade" ASME-GT2003-38303, ASME TURBO EXPO 2003, Atlanta, Georgia.
4. Huang, J., Corke, T.C., Thomas, F.O., 2003, "Plasma Actuators for Separation Control of Low Pressure Turbine Blades," AIAA Paper No. AIAA-2003-1027.
5. Steelant, J., and Dick, E., (2001), "Modeling of Laminar-Turbulent Transition for High Freestream Turbulence," Journal of Fluids Engineering, Vol. 123, pp. 22-30.
6. Menter, F.R., Langtry, R.B., Likki, S.R., Suzen, Y.B., Huang, P.G., and Völker, S., (2004), "A Correlation based Transition Model using Local Variables Part 1 - Model Formulation ASME-GT2004-53452, ASME TURBO EXPO 2004, Vienna, Austria.
7. Menter, F.R., (1994), "Two-equation eddy-viscosity turbulence models for engineering applications", AIAA Journal, Vol. 32, No. 8, pp. 1598-1605.
8. 6" Journal of Fluid Mechanics, Vol. 34, pp. 648-654.
9. Coupland, J., "Separation and Transition over a Semi-Circular Leading edge: T3L Transition Cases", Rolls-Royce Applied Science Laboratory Data, ERCOFTAC Transition Modeling Special Interest Group, http://transition.imse.unige.it/cases/.
10. Zierke, W.C. and Deutsch, S., (1989), "The measurement of boundary layers on a compressor blade in cascade -Vols. 1 and 2", NASA CR 185118.
11. Arts, T., Lambert de Rouvroit, M. and Rutherford, A.W., (1990), "Aero-thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade", von Karman Institute for Fluid Dynamics, Technical Note 174.
12. Schulz, H.D., Gallus, H.D., (1988), "Experimental Investigation of the Three-Dimensional Flow in an Annular Compressor Cascade" ASME Journal of Turbomachinery, Vol. 110, October.
13. Wang, M., Catalano, P. and Iccarino, G., (2001), "Prediction of High Reynolds Number Flow over a Circular Cylinder using LES with Wall Modeling,", Center for Turbulence Annual Research Briefs.