Film cooling and aerodynamic performances of a turbine nozzle guide vane with trenched cooling holes
Author:
Funder
Collaborative Innovation Center of Advanced Aero-Engine, Beihang University
Publisher
Elsevier BV
Subject
Industrial and Manufacturing Engineering,Energy Engineering and Power Technology
Reference37 articles.
1. Experimental and numerical studies on film cooling of a corrugated surface;Kuldeep;Appl. Therm. Eng.,2016
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3. A review of turbine shaped film cooling technology;Bunker;J. Heat Transf.,2005
4. A. Dhungel, Y. Lu, A. Phillips, S. Ekkad, J. Heidmann, Film Cooling from a Row of Holes Supplemented with Anti-Vortex Holes, ASME Paper No. GT2007-27419, 2007.
5. D. Rigby, J. Heidmann, Improved Film Cooling Effectiveness by Placing a Vortex Generator Downstream of Each Hole, ASME Paper No. GT2008-51361, 2008.
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