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kw.\*:("Turbine stage")

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Flow through a repeating stage in an axial compressor: A reconsiderationHORLOCK, J. H.Journal of turbomachinery. 2004, Vol 126, Num 4, pp 677-679, issn 0889-504X, 3 p.Article

INFLUENCE DE LA DISTANCE ENTRE LES ETAGES DE TURBINE SUR LE FONCTIONNEMENT DU COMPARTIMENT DE PRELEVEMENTGOGOLEV IG; PEREVEZENTSEV VT; MARKOV K YA et al.1982; TEPLOENERGETIKA (MOSK., 1954); ISSN 0040-3636; SUN; DA. 1982; NO 3; PP. 56-58; BIBL. 4 REF.Article

OPERATING CONDITIONS OF TWO-STAGE STEAM TURBINESGOGOLEV IG; GOGOLEVA EI.1979; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; BYS; DA. 1979; VOL. 22; NO 11; PP. 50-55; BIBL. 1 REF.Article

Influence de l'ouverture méridienne sur le rendement d'un étage de turbine à gazLASENKO, K. M; ROSKOSHNYJ, N. V; SARANTSEV, K. B et al.Energo-mašinostroenie. 1985, Num 2, pp 4-7Article

Détermination théorique et expérimentale des pertes d'entrée dans l'étape de la TurbineSAMOJLOVICH, G. S; AFONIN, M. V; BARRIENTOS, K. A et al.Teploenergetika (Moskva, 1954). 1984, Num 2, pp 66-67, issn 0040-3636Article

DAS WIRKUNGSGRADVERHALTEN VOLL- UND TEILBEAUFSCHLAGTER STUFEN BZW. STUFENGRUPPEN BEI ABWEICHUNG VOM AUSLEGUNGSPUNKT. = THE EFFICIENCY BEHAVIOUR OF FULLY OR PARTLY ADMITTED STAGES OR STAGE SETS IN CASE OF DEVIATION FROM THE DESIGN POINT = L'EFFICIENCE D'ETAGES OU DE GROUPES D'ETAGES ALIMENTES ENTIEREMENT OU PARTIELLEMENT EN CAS D'ECART DE LA VALEUR PREVUEGERNHARDT A.1977; ENERGIETECHNIK; DTSCH.; DA. 1977; VOL. 27; NO 2; PP. 63-66; BIBL. 4 REF.Article

STUDY OF THE OPERATION CONDITIONS OF THE HEAT RECOVERY STEAM TURBINE LAST STAGES WITH DIFFERENT VOLUMETRIC FLOW RATESSHAPIRO GA; ZAKHAROV YU V; LAGUN VP et al.1976; TEPLOENERGETIKA; S.S.S.R.; DA. 1976; NO 7; PP. 65-68; BIBL. 6 REF.Article

SELECTION OF OPTIMAL ELEMENTARY STAGE PARAMETERS FOR GIVEN VALUES OF U/CO AND CZBOJKO AV; GOVORUSHCHENKO YU N.1977; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; S.S.S.R.; DA. 1977; NO 5; PP. 65-70; BIBL. 6 REF.Article

ANALYTICAL METHOD FOR LAST STAGE PARAMETERS OPTIMIZATION, WITH ENERGY LOSS IN EXIT FLOW MINIMIZATIONSHUBENKO SHUBIN LA; POZNAKHIREV VF; ANTIPTSEV YU P et al.1976; TEPLOENERGETIKA; S.S.S.R.; DA. 1976; NO 7; PP. 61-65; BIBL. 2 REF.Article

L'optimisation des parties basse pression des turbines thermiquesLAPSHIN, K. L.Teploenergetika (Moskva, 1954). 1989, Num 2, pp 18-21, issn 0040-3636Article

Les principes de l'étude aérodynamique des étapes de turbines à charge élevée, pour les turbines à gaz fixesKIRILLOV, I. I; LAPSHIN, K. L; SALIVON, N. D et al.Energo-mašinostroenie. 1985, Num 2, pp 2-3Article

Determination of the theoretical head of a centrifugal pump or compressor stageSHERSTYUK, A. N; EROFEEV, R. A.Chemical and petroleum engineering. 2001, Vol 37, Num 3-4, pp 154-157, issn 0009-2355Article

Effet de l'inhomogénéité du flux dans la chambre de prélèvement et dans la tubulure d'échappement sur les caractéristiques non stationnaires d'un étage de turbineGNESIN, V. I; SOLODOV, V. G.Teploenergetika (Moskva, 1954). 1988, Num 4, pp 22-26, issn 0040-3636Article

Modernisation du diaphragme du dernier étage de la turbine K-160-130SIMOYU, L. L; LAGUN, V. P; INDURSKIJ, M. S et al.Teploenergetika (Moskva, 1954). 1986, Num 6, pp 26-30, issn 0040-3636Article

Errata to Analysis on the Effect of a Nonuniform Inlet Profile on Heat Transfer and Fluid Flow in Turbine Stages [Journal of Turbomachinery, 134(1), 011012]SALVADORI, Simone; MONTOMOLI, Francesco; MARTELLI, Francesco et al.Journal of turbomachinery. 2013, Vol 135, Num 5, issn 0889-504X, p. 057001.1Article

Einfluss der Ein- und Austrittsstutzen auf die Charakteristiken einer Turbinenstufe = Effet des connexions d'entrée et de sortie sur la caractérisation d'un étage de turbine = Influence of inlet and outlet connections on the characterics of steam turbine stageDROKONOV, A. M.Energietechnik. 1989, Vol 39, Num 3, pp 81-84, issn 0013-7421Article

Verluste durch Sekundärströmungen in axialen Turbinenstufen = Losses caused by secondary flows in axial turbine stagesSAUER, H; SEIDEL, G.Maschinenbautechnik. 1991, Vol 40, Num 3, pp 118-124, issn 0025-4495Article

Selection of the optimal alternative for the partial stage of a turbinePOSETSEL'SKII, A. A; LAPSHIN, K. L.Thermal engineering. 1998, Vol 45, Num 1, pp 81-83, issn 0040-6015Article

Experimental investigation and performance analysis of six low flow coefficient centrifugal compressor stagesPAROUBEK, J; CYRUS, V; KYNCL, J et al.Journal of turbomachinery. 1995, Vol 117, Num 4, pp 585-592, issn 0889-504XConference Paper

Untersuchungen an einer Turbinen-Modellstufe mit Regulierleitrad = Examinations at a turbine model stage with a regulating guide diskBOOS, P.Maschinenbautechnik. 1991, Vol 40, Num 3, pp 109-112, issn 0025-4495Article

Problèmes de conception des étages de turbines axialesBOJKO, A. V; GOVORUSHCHENKO, YU. N.Izvestiâ Akademii nauk SSSR. Ènergetika i transport. 1985, Num 3, pp 134-140, issn 0002-3310Article

STUDY OF THE ENTHALPY DROP DISTRIBUTION IN A TURBINE TWO-COMPARTMENT STAGEGOGOLEV IG; GOGOLEVA EI.1980; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; BYS; DA. 1980; VOL. 23; NO 3; PP. 51-57Article

INFLUENCE OF STEAM CONDENSATION ON FLOW CHARACTERISTICS IN TURBINE STAGEFILIPPOV GA; SELEZNEV LI; GORDEEVA IV et al.1976; ENERGO-MASHINOSTR.; S.S.S.R.; DA. 1976; NO 6; PP. 21-23; BIBL. 8 REF.Article

EXPERIMENTAL STUDY OF A HIGHLY LOADED TURBINE STAGEIGNAT'EVSKIJ EA; KONSTANTINOV YU A; LAZAREV L YA et al.1976; TRUDY MOSKOV. ENERGET. INST.; S.S.S.R.; DA. 1976; NO 306; PP. 99-105; BIBL. 2 REF.Article

Reduction of nonuniformity of flow parameters at an inlet to a nozzle row of the first uncontrolled stage of a steam turbine with partial steam admissionZARYANKIN, A. E; ZROICHIKOV, N. A; ARIANOV, S. V et al.Thermal engineering. 2006, Vol 53, Num 11, pp 862-867, issn 0040-6015, 6 p.Article

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