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Results 1 to 25 of 996

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Effect of shock waves on supersonic film cooling with a slotted wallWEI PENG; JIANG, Pei-Xue.Applied thermal engineering. 2014, Vol 62, Num 1, pp 187-196, issn 1359-4311, 10 p.Article

Internal wall-jet film cooling with compound angle cylindrical holesSHINE, S. R; SUNIL KUMAR, S; SURESH, B. N et al.Energy conversion and management. 2013, Vol 68, pp 54-62, issn 0196-8904, 9 p.Article

Overall Effectiveness of a Blade Endwall With Jet Impingement and Film CoolingMENSCH, Amy; THOLE, Karen A.Journal of engineering for gas turbines and power. 2014, Vol 136, Num 3, issn 0742-4795, 031901.1-031901.10Article

Film cooling on a gas turbine blade suction side with converging slot-holeYU YAO; ZHANG, Jing-Zhou; WANG, Li-Ping et al.International journal of thermal sciences. 2013, Vol 65, pp 267-279, issn 1290-0729, 13 p.Article

Film cooling effectiveness: Comparison of adiabatic and conjugate heat transfer CFD modelsSILIETI, Mahmood; KASSAB, Alain J; DIVO, Eduardo et al.International journal of thermal sciences. 2009, Vol 48, Num 12, pp 2237-2248, issn 1290-0729, 12 p.Article

Film cooling performance and heat transfer over an inclined film-cooled surface at different convergent angles with respect to highly turbulent mainstreamYANG, C. S; LIN, C. L; GAU, C et al.Applied thermal engineering. 2009, Vol 29, Num 1, pp 167-177, issn 1359-4311, 11 p.Article

Experimental investigation on heat transfer characteristics of film cooling using parallel-inlet holesWEIHUA YANG; XUE LIU; GUOHUI LI et al.International journal of thermal sciences. 2012, Vol 60, pp 32-40, issn 1290-0729, 9 p.Article

Film cooling performance and heat transfer over an inclined film-cooled surface at different divergent angles with respect to highly turbulent mainstreamYANG, Chih-Sheng; LIN, C. L; GAU, C et al.Experimental thermal and fluid science. 2008, Vol 32, Num 6, pp 1313-1321, issn 0894-1777, 9 p.Article

Numerical investigation of film cooling effectiveness on the curved surfaceKOC, I; PARMAKSIZOGLU, C; CAKAN, M et al.Energy conversion and management. 2006, Vol 47, Num 9-10, pp 1231-1246, issn 0196-8904, 16 p.Article

Numerical simulation on impingement and film composite cooling of blade leading edge model for gas turbineZHAO LIU; LV YE; CHANGYEE WANG et al.Applied thermal engineering. 2014, Vol 73, Num 2, pp 1432-1443, issn 1359-4311, 12 p.Conference Paper

Experimental flow field investigations of a film cooling hole featuring an orificeYINGJIE ZHENG; IBRAHIM HASSAN.Applied thermal engineering. 2014, Vol 62, Num 2, pp 766-776, issn 1359-4311, 11 p.Article

Three-dimensional analysis of temperature field for various parameters affect the film cooling effectivenessBAYRAKTAR, Seyfettin; YILMAZ, Tamer.Energy conversion and management. 2011, Vol 52, Num 4, pp 1914-1929, issn 0196-8904, 16 p.Article

Film-cooling effectiveness downstream of a single row of holes with variable density ratioSINHA, A. K; BOGARD, D. G; CRAWFORD, M. E et al.Journal of turbomachinery. 1991, Vol 113, Num 3, pp 442-449, issn 0889-504XArticle

Computational study of film cooling from single and two staggered rows of novel semi-circular cooling holes including coolant plenumASGHAR, F. H; HYDER, M. J.Energy conversion and management. 2011, Vol 52, Num 1, pp 329-334, issn 0196-8904, 6 p.Article

Influence of Large Wake Disturbances Shed From the Combustor Wall on the Leading Edge Film CoolingMAZZONI, Cosimo Maria; KLOSTERMEIER, Christian; ROSIC, Budimir et al.Journal of engineering for gas turbines and power. 2014, Vol 136, Num 8, issn 0742-4795, 081503.1-081503.13Article

Flow visualization and film cooling effectiveness measurement around shaped holes with compound angleLEE, H-W; PARK, J. J; LEE, J. S et al.The data science library. 2000, pp 45-50, isbn 2-84299-207-5Conference Paper

Heat transfer and film cooling effectiveness on the squealer tip of a turbine bladeJUN SU PARK; DONG HYUN LEE; RHEE, Dong-Ho et al.Energy (Oxford). 2014, Vol 72, pp 331-343, issn 0360-5442, 13 p.Article

Effects of density ratio on the hydrodynamics of film coolingPIETRZYK, J. R; BOGARD, D. G; CRAWFORD, M. E et al.Journal of turbomachinery. 1990, Vol 112, Num 3, pp 437-443, issn 0889-504X, 7 p.Conference Paper

Effect of Film Cooling on Turbine CapacityPOVEY, T.Journal of engineering for gas turbines and power. 2010, Vol 132, Num 1, issn 0742-4795, 011901.1-011901.10Article

Théorie du refroidissement par film d'un support massifNABEREZHNYKH, V. P; SELYAKOV, B. I; FEL'DMAN, EH. P et al.Inženerno-fizičeskij žurnal. 1984, Vol 47, Num 4, issn 0021-0285, 677Article

Banc d'essai pour grilles d'aubes de turbine à gaz refroidies par film d'airITEN, P; BAUMANN, W; GROB, D et al.La Technique moderne (Paris. 1908). 1983, Vol 75, Num 5-6, pp 18-24, issn 0040-1250Article

Prediction of film cooling with a liquid coolantSHEMBHARKAR, T. R; PAI, B. R.International journal of heat and mass transfer. 1986, Vol 29, Num 6, pp 899-908, issn 0017-9310Article

Calcul de l'efficacité du refroidissement d'une plaque par injection oblique du fluide de refroidissement par rapport à l'écoulement principal en tenant compte de la zone d'arrêtKORTIKOV, N. N; SMIRNOV, YU. A.Inženerno-fizičeskij žurnal. 1985, Vol 48, Num 5, pp 715-719, issn 0021-0285Article

Performance Evaluation of a Novel Film-Cooling HoleLEE, Ki-Don; KIM, Kwang-Yong.Journal of heat transfer. 2012, Vol 134, Num 10, issn 0022-1481, 101702.1-101702.7Article

Experimental investigation of heat transfer characteristics in a variable cross-sectioned two-pass channel with combined film cooling holes and inclined ribsXIANGYUN LIU; ZHI TAO; SHUITING DING et al.Applied thermal engineering. 2013, Vol 50, Num 1, pp 1186-1193, issn 1359-4311, 8 p.Article

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