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 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

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

SELECTION OF OPTIMAL ELEMENTARY STAGE PARAMETERS FOR GIVEN VALUES OF U/C_O AND C_ZBOJKO 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

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

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

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

Refroidissement des turbines à gaz: Techniques et efficacitéFACCHINI, Bruno; INNOCENTI, Luca.Techniques de l'ingénieur. Génie mécanique. 2005, Vol BL4, Num BM4566, issn 1762-8768, BM4566.1-BM4566.24Article

Kühlung transsonischer Turbinenstufen mittels unterexpandierter Kühlfilme = Transonic turbine stage cooling by underexpanded cooling filmsMOSER, S; WOISETSCHLÄGER, J; MAYRHOFER, N et al.VDI-Berichte. 2000, pp 125-138, issn 0083-5560, isbn 3-18-091566-8Conference Paper

Bottom Steam Turbines of the Ural Turbine WorksBARINBERG, G. D; VALAMIN, A. E; SAKHNIN, Yu. A et al.Thermal engineering. 2008, Vol 55, Num 8, pp 665-671, issn 0040-6015, 7 p.Article

Last Stage Performance Considerations in Low-Pressure Turbines of Power Plants : A Case StudySUNDER RAJ, Komandur S.Journal of engineering for gas turbines and power. 2008, Vol 130, Num 2, issn 0742-4795, 023004.1-023004.7Article

Bigger blades cut costsMUJEZINOVIC, Amir.Modern power systems. 2003, Num FEV, pp 25-27, issn 0260-7840, 2 p.Article

The specifics of erosion wear of the working blades in the last stages of turbines with a capacity of 300 MW and higherAVERKINA, N. V; DOLGOPLOSK, E. P; KACHURINER, Yu. Ya et al.Thermal engineering. 2001, Vol 48, Num 11, pp 915-922, issn 0040-6015Article

Activité chimique des gaz de combustion au cours de la détente dans les futures turbines à gaz = Chemically reactife flox of hot combustion gases in the expansion turbine of future gas turbinesGodin, Thierry; Stouffes, P.1996, 170 p.Thesis

Automatizatsiya proektno-tekhnologicheskikh rabot pri sozdanii poslednej stupeni turbomashinSHUBENKO-SHUBNI, L. A; TARELIN, A. A.Ènergomašinostroenie. 1989, Num 10, pp 42-46, issn 0131-1336Article

Research on characteristics of varying conditions for nozzle governing stage based on dimensional analysisXU, Jian-Qun; LIN MA; SUN, You-Yuan et al.Energy (Oxford). 2014, Vol 65, pp 590-595, issn 0360-5442, 6 p.Article