Arrangement effects of inclined teardrop-shaped dimples on film cooling performance of dimpled cutback surface at airfoil trailing edge

Author:

Murata Akira,Yano Kohta,Hanai Masaki,Saito Hiroshi,Iwamoto Kaoru

Funder

JSPS KAKENHI

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference23 articles.

1. Trailing-edge cooling for gas turbines;Cunha;J. Propul. Power,2006

2. An experimental investigation of film cooling effectiveness for slots of various exit geometries;Taslim;AIAA J. Thermophys. Heat Transf.,1992

3. P. Martini, A. Schulz, H.-J. Bauer, C.F. Whitney, Detached Eddy simulation of film cooling performance on the trailing edge cut-back of gas turbine airfoils, ASME Paper, GT2005-68084, 2005.

4. S. Ravelli, G. Barigozzi, Application of unsteady CFD methods to trailing edge cutback film cooling, in: Proc. of ASME Turbo Expo 2014, June 16–20, 2014, Dusseldorf, Germany, GT2014-25435, p. 14, 2014.

5. H. Schneider, H.J. Bauer, D. von Terzi, W. Rodi, Coherent structures in trailing-edge cooling and the challenge for turbulent heat transfer modelling, in: Proc. of ASME Turbo Expo 2012, June 11–15, 2012, Copenhagen, Denmark, GT2012-69771, 2012.

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