Discussions of some myths and concerned practices of film cooling research

作者: Ting Wang , Lei Zhao

DOI: 10.1016/J.IJHEATMASSTRANSFER.2010.11.003

关键词:

摘要: Abstract This paper focuses on discussing four myths and concerned conventional practices of film cooling research guided by a series computational simulations. The issues that have been discussed include: (a) the effectiveness (φ) is given constant (0.6) to calculate heat flux ratio HFR = q ″ / o between film-cooled no-film cases; (b) adiabatic wall temperature driving cooling; (c) transfer coefficient can be obtained from an isoenergetic experiment (Tj = Tg); (d) using heated surface provide simplified approach simulate film-cooling condition. result shows not always (i.e. Taw larger than Tw), but does act well as reference in correctly predicting direction giving positive coefficient. Using value for φ questionable may lead un-realistic or false HFR. equation was theoretically exact error up 20%. A revised provided this paper. dominant energy passage turbine airfoil hot combustion gas flows into airfoil; therefore, employing boundary condition with hotter main stream flow cold injection actual found fundamentally questionable. conjugate simulation includes internal reversed blade gives negative possible, due conduction downstream region near hole cooler region.

参考文章(15)
B. E. Launder, D. B. Spalding, Lectures in mathematical models of turbulence ,(1972)
patrick h. oosthuizen, david naylor, Introduction to Convective Heat Transfer Analysis ,(1998)
W. J. Mick, R. E. Mayle, Stagnation Film Cooling and Heat Transfer, Including Its Effect Within the Hole Pattern Journal of Turbomachinery-transactions of The Asme. ,vol. 110, pp. 66- 72 ,(1988) , 10.1115/1.3262169
Sarah M Coulthard, Ralph J Volino, Karen A Flack, None, Effect of Jet Pulsing on Film Cooling—Part II: Heat Transfer Results Journal of Turbomachinery-transactions of The Asme. ,vol. 129, pp. 247- 257 ,(2007) , 10.1115/1.2437230
S. Ou, J. C. Han, Influence of mainstream turbulence on leading edge film cooling heat transfer through two rows of inclined film slots Journal of Turbomachinery-transactions of The Asme. ,vol. 114, pp. 724- 733 ,(1992) , 10.1115/1.2928025
Katharine L. Harrison, David G. Bogard, Use of the Adiabatic Wall Temperature in Film Cooling to Predict Wall Heat Flux and Temperature ASME Turbo Expo 2008: Power for Land, Sea, and Air. pp. 1197- 1207 ,(2008) , 10.1115/GT2008-51424
Brian D. Mouzon, Elon J. Terrell, Jason E. Albert, David G. Bogard, Net Heat Flux Reduction and Overall Effectiveness for a Turbine Blade Leading Edge ASME Turbo Expo 2005 - Gas Turbie Technology: Focus for the Future. pp. 825- 832 ,(2005) , 10.1115/GT2005-69002
B. Sen, D. L. Schmidt, D. G. Bogard, Film Cooling With Compound Angle Holes: Heat Transfer Journal of Turbomachinery-transactions of The Asme. ,vol. 118, pp. 800- 806 ,(1996) , 10.1115/1.2840937
M. Wolfshtein, The velocity and temperature distribution in one-dimensional flow with turbulence augmentation and pressure gradient International Journal of Heat and Mass Transfer. ,vol. 12, pp. 301- 318 ,(1969) , 10.1016/0017-9310(69)90012-X
Yiping Lu, Alok Dhungel, Srinath V. Ekkad, Ronald S. Bunker, Effect of Trench Width and Depth on Film Cooling From Cylindrical Holes Embedded in Trenches Journal of Turbomachinery-transactions of The Asme. ,vol. 131, pp. 011003- ,(2009) , 10.1115/1.2950057