Film cooling on a gas turbine blade pressure side or suction side with axial shaped holes
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference23 articles.
1. Effects of hole geometry and density on three-dimensional film cooling;Goldstein;Int. J. Heat Mass Transfer,1974
2. K. Thole, M. Gritsch, A. Schulz, S. Wittig, Flowfield measurements for film cooling holes with expanded exits, ASME Paper No. 96-GT-174, 1996.
3. M. Gritsch, A. Schulz, S. Wittig, Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits, ASME Paper No. 97-GT-164, 1997.
4. Y. Yu, C.-H. Yen, T.I.-P. Shih, M.K. Chyu, S. Gogineni, Film cooling effectiveness and heat transfer coefficient distributions around diffusion shaped holes, ASME Paper No. 99-GT-34, 1999.
5. D.L. Schmidt, B. Sen, D.G. Bogard, Film cooling with compound angle holes: adiabatic effectiveness, ASME Paper No. 94-GT-312, 1994.
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