Transition modelling implications in the CFD analysis of a turbine nozzle vane cascade tested over a range of Mach and Reynolds numbers

Author:

Marconcini Michele,Pacciani Roberto,Arnone Andrea

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference21 articles.

1. B. J. Abu Ghannam and R. Shaw. Natural Transition of Boundary Layers–The Effect of Turbulence, Pressure Gradient and Flow History. Journal of Mechanical Engineering Science, 22(5): 213–228, 1980.

2. A. Arnone. Viscous Analysis of Three–Dimensional Rotor Flow Using a Multigrid Method. J. Turbomach., 116(3): 435–445, July 1994.

3. A. Arnone, M. S. Liou, and L. A. Povinelli. Navier–Stokes Solution of Transonic Cascade Flow Using Non–Periodic C–Type Grids. J. Propul. Power, 8(2): 410–417, March–April 1992.

4. T. Arts, M. Lambert de Rouvroit, and A. W. Rutherford. Aero–Thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade. Technical note 174, von Kármán Institute, Brussels, Belgium, 1990.

5. G. Barigozzi and S. Ravelli. Effects of Trailing Edge Film Cooling on the Aerodynamic Performance of a Nozzle Vane Cascade. 9th European Turbomach. Conf., Istanbul, Turkey, pages 437–447, 2011.

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