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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

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

ON CALCULATING THE EFFECTIVENESS OF FILM COOLING OF A FLAT PLATE = CALCUL DE L'EFFICACITE DU REFROIDISSEMENT PELLICULAIRE D'UNE PLAQUE PLATEREPUKHOV VM.1973; HEAT TRANSFER, SOVIET RES.; U.S.A.; DA. 1973; VOL. 5; NO 1; PP. 177-183; BIBL. 12 REF.Serial Issue

EFFICACITE DU REFROIDISSEMENT PAR FILM AVEC GRADIENT DE PRESSION LONGITUDINAL FAVORABLEZYSIN VA; ZOLOTOGOROV MS; GRANOVSKIJ VS et al.1972; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1972; VOL. 23; NO 6; PP. 1001-1007; ABS. ANGL.; BIBL. 12 REF.Serial Issue

L'ECHANGE DE CHALEUR, DANS LE SOUFFLAGE, PAR JET, DU BORD D'ENTREE DES AUBES DE TURBINEDYBAN EP; EHPIK EH YA; MAZUR AI et al.1972; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; S.S.S.R.; DA. 1972; VOL. 15; NO 5; PP. 90-96; BIBL. 6 REF.Serial Issue

A STUDY OF FILM-COOLING EFFECTIVENESS OF SOME GAS-TURBINE STATOR SURFACES = ETUDE DE L'EFFICACITE DU REFROIDISSEMENT PAR FILM DE QUELQUES SURFACES DE STATOR DE TURBINE A GAZZYSIN VA; ZOLOTOGOROV MS.1972; HEAT TRANSFER, SOVIET RES.; U.S.A.; DA. 1972; VOL. 4; NO 3; PP. 6-10; BIBL. 4 REF.Serial Issue

PREDICTED FILM COOLING NEAR FLUSH SLOTS-COMPARISON WITH EXPERIMENTMETZGER DE; CARPER HJ JR; WARREN JM et al.1972; IN: AIAA 7TH THERMOPHYS. CONF. SAN ANTONIO, TEX., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1972; VOL. 291; PP. 1-10; BIBL. 16 REF.Conference 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

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

HEAT CONDUCTION AND HYDRODYNAMIC LIMITATIONS TO SIMPLE REWETTING PROCESSES.GROLMES MA.1976; IN: TWO PHASE FLOW HEAT TRANSFER SYMP.-WORKSHOP. PROC.; FORT LANDERDALE, FLA.; 1976; CORAL GABLES; UNIV. MIAMI; DA. 1976; PP. 99-102; BIBL. 8 REF.Conference Paper

FILM COLLING FOR HIGH TEMPERATURE TURBINES = REFROIDISSEMENT PAR FILM POUR TURBINES A HAUTE TEMPERATUREFERRI A.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 525; PP. 1-11; BIBL. 13 REF.Conference Paper

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EFFICIENCY OF GAS TURBINE BLADING FILM COOLINGBOGOMOLOV EN; PIOTUKH SM.1978; TEPLOENERGETIKA; S.S.S.R.; DA. 1978; NO 1; PP. 9-12; BIBL. 11 REF.Article

PRACTICAL METHOD OF CALCULATING THE PROCESSES OF GAS EXPANSION WITH FRICTION AND EXTERNAL HEAT TRANSFERMARIEV DI.1975; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; S.S.S.R.; DA. 1975; VOL. 18; NO 12; PP. 81-86; BIBL. 2 REF.Article

EXPERIMENTAL INVESTIGATION OF FILM COOLING OF EXIT EDGES OF STATIONARY BLADINGYEFIMCHUK LA; ZUBAREV AP; BLYUMIN YA I et al.1973; HEAT TRANSFER, SOVIET RES.; U.S.A.; DA. 1973; VOL. 5; NO 3; PP. 126-129; BIBL. 2 REF.Serial Issue

Film cooling measurements for novel hole configurationsYIPING LU; NASIR, Hasan; FAUCHEAUX, David et al.Journal of heat transfer. 2006, Vol 128, Num 8, pp 737-737, issn 0022-1481, 1 p.Article

Effects of the condition of the approach boundary layer and of mainstream pressure gradients on the heat transfer coefficient on film-cooled surfacesHAY, N; LAMPARD, D; SALUJA, C. L et al.Journal of engineering for gas turbines and power. 1985, Vol 107, Num 1, pp 99-104, issn 0742-4795Conference Paper

Cooling airflow studies at the leading edge of a film-cooled airfoilTILLMAN, E. S; JEN, H. F.Journal of engineering for power. 1984, Vol 106, Num 1, pp 214-221, issn 0022-0825Article

The effect of temperature ratios on the film cooling processLOFTUS, P. J; JONES, T. V.Journal of engineering for power. 1983, Vol 105, Num 3, pp 615-620, issn 0022-0825Article

Film cooling effectiveness on a turbine bladeGOLDSTEIN, R. J; KORNBLUM, Y; ECKERT, E. R. G et al.Israel Journal of Technology. 1982, Vol 20, Num 4-5, pp 193-200, issn 0021-2202Article

Theoretical estimation of the optimum glass cover water film cooling parameters combinations of a stepped solar stillEL-SAMADONY, Y. A. F; KABEEL, A. E.Energy (Oxford). 2014, Vol 68, pp 744-750, issn 0360-5442, 7 p.Article

Convective heat transfer models for three-temperatures problems application to jet impingement and film coolingBREVET, P; DORIGNAC, E; PETRE, B et al.International heat transfer conference. 2002, pp 345-350, isbn 2-84299-308-X, 6 p.Conference Paper