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

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

BREVET 2.350.568 (A1) (77 03217). - 4 FEVRIER 1977. PANNEAU DE RUISSELLEMENT DE TOUR DE REFROIDISSEMENT.sdPatent

COOLING SUPERHEATED SURFACES BY A DOWNFLOWING LIQUID FILMIVANOV VG; KOZLOV VM; MUSVIK AB et al.1983; INZENERNO-FIZICESKIJ ZURNAL; ISSN 0021-0285; BYS; DA. 1983; VOL. 44; NO 3; PP. 383-390; ABS. ENG; BIBL. 13 REF.Article

EFFICIENCY OF HEAT PROTECTIVE CURTAINSHISHOV EV.1976; P.M.T.F.; S.S.S.R.; DA. 1976; PP. 100-103; BIBL. 3 REF.Article

INVESTIGATION OF FILM COOLING EFFICIENCY WITH INJECTION THROUGH A SINGLE OPENINGALEKSEYEV NM; ZELENGUR AA.1981; HEAT TRANSFER. SOV. RES.; ISSN 0440-5749; USA; DA. 1981; VOL. 12; NO 5; PP. 31-41; BIBL. 9 REF.Article

STUDY OF SOME PECULARITIES OF FILM COOLING OF GUIDE AND MOVING BLADINGPIOTUKH SM.1979; TEPLOENERGETIKA (MOSK., 1954); ISSN 0040-3636; SUN; DA. 1979; NO 11; PP. 37-41; BIBL. 5 REF.Article

APPLICATION OF FORMAL OPTIMIZATION PROCEDURES TO FILM COOLING DESIGNHEDRICK JK; METZGER DE; TAKEUCHI DT et al.1978; J. ENERGY; USA; DA. 1978; VOL. 2; NO 4; PP. 210-215; BIBL. 11 REF.Article

THE EFFECT OF BULK FLOW TWIST ON THE EFFICIENCY OF FILM HEATING IN AXISYMMETRIC FLOW AROUND A CYLINDER.REPUKHOV VM; BOGACHUK KOZACHUK KA.1975; HEAT TRANSFER, SOVIET RES.; U.S.A.; DA. 1975; VOL. 7; NO 6; PP. 54-59; BIBL. 3 REF.Article

THE INFLUENCE OF A LAMINAR BOUNDARY LAYER AND LAMINAR INJECTION ON FILM COOLING PERFORMANCEGOLDSTEIN RJ; YOSHIDA T.1982; J. HEAT TRANSFER; ISSN 0022-1481; USA; DA. 1982; VOL. 104; NO 2; PP. 355-362; BIBL. 25 REF.Article

NUMERICAL STUDY OF THE DEPENDENCE OF FILM COOLING OF PERFORATED BLADES OF GAZ TURBINES FROM NETWORK PARAMETERSBOGOMOLOV EN; ORLOVA VI.1982; IZVESTIJA VYSSIH UCEBNYH ZAVEDENIJ. ENERGETIKA; ISSN 0579-2983; BYS; DA. 1982; NO 10; PP. 50-56; BIBL. 3 REF.Article

BREVET. DISPOSITIF DE REGULARISATION DU RUISSELLEMENT D'UN LIQUIDE SUR UNE SURFACE, TELLE QUE CELLE DES PLAQUES D'UN ECHANGEUR DE TEMPERATURE A RUISSELLEMENT DE LIQUIDE1980; ; FRA; DA. 1980-03-21; FR/A1/2.431.670; DEP.78-21116/1978-07-17Patent

ACCOUNT OF FILM TURBULENCE FOR PREDICTING FILM COOLING EFFECTIVEMENT IN GAS TURBINE COMBUSTORSSTURGESS GJ.1980; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1980; VOL. 102; NO 3; PP. 524-534; BIBL. 13 REF.Article

BREVET ELEMENT ECHANGEUR TRIDIMENSIONNEL POUR LE GUIDAGE DE LIQUIDE DANS DES INSTALLATIONS DE CONTACT LIQUIDE-GAZ, EN PARTICULIER POUR LES TOURS DE REFRIGERATION1979; ; FRA; DA. 1979-02-16; FR/A1/2.394.778; DEP.78 17669/1978-06-13; PR. DE/P27 26 723.8/1977-06-14Patent

FILM COOLING OF HEATED TURBINE SURFACES AT SIMULATED CONDITIONSRICHARDS BE; APPELS C; VILLE JP et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. SOCIETY OF AUTOMOTIVE ENGINEERS PROPULSION CONFERENCE. 13/1977/ORLANDO FL; USA; NEW YORK: AIAA; DA. 1978; VOL. 947; PP. 7 P.; BIBL. 13 REF.Conference Paper

ANALYSIS OF SUBSONIC FLOW OF A COMPRESSIBLE FLUID IN CONFLUENCE CHANNELS AND ITS APPLICATION FOR THEORETICAL CONSIDERATIONS ON FILM COOLING IN HIGH-TEMPERATURE GAS TURBINESKOREMATSU K.1977; J. MECH. ENGNG LAB.; JAP.; DA. 1977; VOL. 31; NO 2; PP. 85-92; ABS. ANGL.; BIBL. 6 REF.Article

TWO-DIMENSIONAL ANALYSIS OF CONDUCTION-CONTROLLED REWETTING WITH PRECURSORY COOLING.DUA SS; TIEN CL.1976; J. HEAT TRANSFER; U.S.A.; DA. 1976; VOL. 98; NO 3; PP. 407-413; BIBL. 21 REF.Article

DOUBLE-ROW DISCRETE-HOLE COOLING: AN EXPERIMENTAL AND NUMERICAL STUDYBERGELES G; GOSMAN AD; LAUNDER BE et al.1980; J. ENGNG POWER; USA; DA. 1980; VOL. 102; NO 2; PP. 498-503; BIBL. 13 REF.Article

AERODYNAMIC LOSS IN A GAS TURBINE STAGE WITH FILM COOLINGITO S; ECKERT ERG; GOLDSTEIN RJ et al.1980; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1980; VOL. 102; NO 4; PP. 964-970; BIBL. 8 REF.Article

EXPERIMENTAL STUDY OF GAS FILM COOLING EFFICIENCIES IN SUPERSONIC AXISYMMETRIC NOZZLESVOLCHKOV EP; KOZ'MENKO VK; LEBEDEV VP et al.1978; HEAT TRANSFER, SOVIET RES.; USA; DA. 1978; VOL. 10; NO 5; PP. 47-56; BIBL. 10 REF.Article

NEW APPROACHES TO TURBINE AIRFOIL COOLING AND MANUFACTURINGSELLERS R; DAHLBERG DE; CALVERT GS et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. SOCIETY OF AUTOMOTIVE ENGINEERS PROPULSION CONFERENCE. 13/1977/ORLANDO FL; USA; NEW YORK: AIAA; DA. 1978; VOL. 948; PP. 8 P.Conference Paper

AIR COOLING OF A TURBINE NOZZLE BLADE OF A STATIONARY GAS TURBINE PLANT AT HIGH PRESSURESVOLODKIN LL.1978; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1978; VOL. 34; NO 5; PP. 897-902; ABS. ANGL.; BIBL. 4 REF.Article

EXPERIMENTAL AND PREDICTED RECOVERY TEMPERATURE DISTRIBUTIONS IN A ROCKET NOZZLE WITH GASEOUS FILM CODING.WILLIAMS JJ; GIEDT WH.1977; J. HEAT TRANSFER; U.S.A.; DA. 1977; VOL. 99; NO 3; PP. 386-391; BIBL. 23 REF.Article

EFFICIENCY OF TURBINE-BLADE COOLING BY AIR INJECTION THROUGH LONGITUDINAL SLOTS.BLYUMIN YI.1976; HEAT TRANSFER, SOVIET RES.; U.S.A.; DA. 1976; VOL. 8; NO 1; PP. 155-160; BIBL. 7 REF.Article

ETUDE DE LA DILUTION SOUS L'EFFET DE L'ACCELERATION CENTRIFUGE DANS UN FOYER A ECOULEMENT GIRATOIRE. = STUDY OF THE DILUTION INDUCED BY THE CENTRIFUGAL ACCELERATION IN A GYRATORY-FLOW COMBUSTORMESTRE A.1976; DGRST-7470726; FR.; DA. 1976; PP. 1-58; BIBL. 4 REF.; (RAPP. FINAL, ACTION CONCERTEE: MEC.)Report