The cause of overprediction of cooling efficiency by unsteady Reynolds averaged simulations of turbine blade trailing edge cooling flow is investigated. This is due to the deficiency in the level of unsteady coherent energy very near to the wall. Farther from the wall, the Reynolds averaged simulation produces the correct level of mixing. Eddy simulations of the instantaneous turbulent eddying produce a close agreement to data on film effectiveness. In particular, they reproduce the reduction in cooling effectiveness toward the trailing edge that has been seen in experiments. The scale adaptive simulation model of Menter and Egorov (2005, “A Scale-Adaptive Simulation Modeling Using Two-Equation Models,” AIAA Paper No. 2005-1095) is invoked for the eddy simulations.
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February 2009
Research Papers
Simulation of Turbine Blade Trailing Edge Cooling
Jongwook Joo,
Jongwook Joo
Aerospace Engineering, Howe Hall,
Iowa State University
, Ames, IA 50011
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Paul Durbin
Paul Durbin
Aerospace Engineering, Howe Hall,
Iowa State University
, Ames, IA 50011
Search for other works by this author on:
Jongwook Joo
Aerospace Engineering, Howe Hall,
Iowa State University
, Ames, IA 50011
Paul Durbin
Aerospace Engineering, Howe Hall,
Iowa State University
, Ames, IA 50011J. Fluids Eng. Feb 2009, 131(2): 021102 (14 pages)
Published Online: January 9, 2009
Article history
Received:
May 7, 2008
Revised:
October 23, 2008
Published:
January 9, 2009
Citation
Joo, J., and Durbin, P. (January 9, 2009). "Simulation of Turbine Blade Trailing Edge Cooling." ASME. J. Fluids Eng. February 2009; 131(2): 021102. https://doi.org/10.1115/1.3054287
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