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COUPLED COMPRESSOR-DIFFUSER FLOW INSTABILITY.GREITZER EM.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 3; PP. 233-238; BIBL. 6 REF.Article

SURGE AND ROTATING STALL IN AXIAL FLOW COMPRESSORS. I. THEORETICAL COMPRESSION SYSTEM MODEL. II. EXPERIMENTAL RESULTS AND COMPARISON WITH THEORY = A COUPS ET DECROCHAGE DANS LES COMPRESSEURS A ECOULEMENT AXIAL. I. MODELE DU SYSTEME DE COMPRESSION THEORIQUE. II. RESULTATS EXPERIMENTAUX ET COMPARAISON AVEC LA THEORIEGREITZER EM.1975; IN: GAS TURBINE CONF. PROD. SHOW; HOUSTON, TEX.; 1975; NEW YORK; AM. SOC. MECH. ENG.; DA. 1975; VOL. 75-GT-9-10; PP. 1-22; BIBL. 13REF.Conference Paper

REVIEW: AXIAL COMPRESSOR STALL PHENOMENAGREITZER EM.1980; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1980; VOL. 102; NO 2; PP. 134-151; BIBL. 80 REF.Article

A NEW EXACT SOLUTION FOR COMPRESSIBLE SWIRLING FLOW.GREITZER EM.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 4; PP. 297-303; BIBL. 6 REF.Article

A SIMPLE MODEL FOR COMPRESSOR STALL CELL PROPAGATIONCUMPSTY NA; GREITZER EM.1982; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1982; VOL. 104; NO 1; PP. 170-176; BIBL. 10 REF.Article

ASYMMETRIC SWIRLING FLOWS IN TURBOMACHINE ANNULIGREITZER EM; STRAND T.1978; J. ENGNG POWER; USA; DA. 1978; VOL. 100; NO 4; PP. 618-629; BIBL. 15 REF.Article

ASYMMETRIC SWIRLING FLOWS IN TURBOMACHINE ANNULIGREITZER EM; STRAND T.1978; GAS TURBINE CONFERENCE/1978-04-09/LONDRES; USA; NEW YORK: ASME; DA. 1978; 12 P.; BIBL. 15 REF.Conference Paper

COMPRESSOR-DIFFUSER INTERACTION WITH CIRCUMFERENTIAL FLOW DISTORTION.GREITZER EM; GRISWOLD HR.1976; J. MECH. ENGNG SCI.; G.B.; DA. 1976; VOL. 18; NO 1; PP. 25-38; BIBL. 16 REF.Article

FLOW FIELD COUPLING BETWEEN COMPRESSION SYSTEM COMPONENTS IN ASYMMETRIC FLOW.GREITZER EM; MAZZAWY RS; FULLKERSON DA et al.1978; J. ENGNG POWER; U.S.A.; DA. 1978; VOL. 100; NO 1; PP. 66-72; BIBL. 10 REF.Article

THE RESPONSE OF TURBOMACHINE BLADES TO LOW FREQUENCY INLET DISTORTIONS.HORLOCK JH; GREITZER EM; HENDERSON RE et al.1977; J. ENGNG POWER; U.S.A.; DA. 1977; VOL. 99; NO 2; PP. 195-203; BIBL. 17 REF.Article

PREDICTION OF COMPRESSOR PERFORMANCE IN ROTATING STALL.DAY IJ; GREITZER EM; CUMPSTY NA et al.1978; J. ENGNG POWER; U.S.A.; DA. 1978; VOL. 100; NO 1; PP. 1-14; BIBL. 17 REF.Article

A ROTATING STALL CONTROL SYSTEM FOR TURBOJET ENGINESLUDWIG GR; NENNI JP; ARNETT SE et al.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 3; PP. 305-314; BIBL. 4 REF.Article

MECHANISM OF INLET-VORTEX FORMATIONDE SIERVI F; VIGUIER HC; GREITZER EM et al.1982; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1982; VOL. 124; PP. 173-207; BIBL. 29 REF.Article

SURGE AND ROTATING STALL IN AXIAL FLOW COMPRESSORS. I. THEORETICAL COMPRESSION SYSTEM MODEL. II. EXPERIMENTAL RESULTS AND COMPARISON WITH THEORY. = POMPAGE ET DECOLLEMENT TOURNANT DANS LES COMPRESSEURS A ECOULEMENT AXIAL. I. MODELE THEORIQUE DU SYSTEME DE COMPRESSION. II. RESULTATS EXPERIMENTAUX ET COMPARAISON AVEC LA THEORIEGREITZER EM; BAMMERT K; MOBARAK A et al.1976; J. ENGNG POWER; U.S.A.; DA. 1976; VOL. 98; NO 2; PP. 190-217; BIBL. DISSEM.Article

THE TIME DOMAIN OF CENTRIFUGAL COMPRESSOR AND PUMP STABILITY AND SURGE.DEAN RC JR; YOUNG LR; BULLOCK RO et al.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 1; PP. 53-63; BIBL. 14 REF.Article

AN EXPERIMENTAL STUDY OF SURGE IN CENTRIFUGAL COMPRESSORS.TOYAMA K; RUNSTADLER PW JR; DEAN RC JR et al.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 1; PP. 115-131; BIBL. 19 REF.Article

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