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STALLING PRESSURE RISE CAPABILITY OF AXIAL FLOW COMPRESSOR STAGESKOCH CC.1981; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1981; VOL. 103; NO 4; PP. 645-656; BIBL. 20 REF.Article

STABILITE DU FONCTIONNEMENT DES COMPRESSEURS DANS LES EQUIPEMENTS ENERGETIQUESPRIVALOV BG.1981; ENERGO-MASHINOSTR.; SUN; DA. 1981; NO 7; PP. 18-19; BIBL. 5 REF.Article

NONLINEAR ANALYSIS OF SURGE CYCLES.GYARMATHY G.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 1; PP. 258-259Article

CONSIDERATIONS FOR THE CONTROL OF SURGE IN DYNAMIC COMPRESSORS USING CLOSE COUPLED RESISTANCES.DUSSOURD JL; PFANNEBECKER G; SINGHANIA SK et al.1976; IN: CENTRIFUGAL COMPRESSOR PUMP STAB. STALL SURGE. CONF.; NEW ORLEANS; 1976; NEW YORK; AM. SOC. MECH. ENG.; DA. 1976; PP. 1-28; BIBL. 9 REF.Conference Paper

UNSTEADY FLOW PHENOMENA IN CENTRIFUGAL FANS. II: THREE DIMENSIONAL UNSTEADY FLOW MEASUREMENTKUBO T.1980; BULL. JSME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 185; PP. 1771-1778; BIBL. 7 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

STUDY OF CASING TREATMENT EFFECTS IN AXIAL FLOW COMPRESSORS.BOYCE MP; SCHILLER RN; DESAI AR et al.1975; J. ENGNG POWER; U.S.A.; DA. 1975; VOL. 97; NO 4; PP. 477-483; BIBL. 4 REF.Article

ANMERKUNGEN ZUR REGELUNG GROSSER TURBOVERDICHTER = REMARQUES SUR LA REGULATION DES GROS TURBOCOMPRESSEURSFASOL KH.1983; BRENNSTOFF-WAERME-KRAFT; ISSN 0006-9612; DEU; DA. 1983; VOL. 35; NO 1-2; PP. 55-61; BIBL. 38 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

EFFECT OF INTAKE CONDITIONS ON SUPERSONIC UNSTALLED FLUTTER IN TURBOFAN ENGINESHALLIWELL DG.1980; J. AIRCR.; USA; DA. 1980; VOL. 17; NO 5; PP. 300-304; BIBL. 6 REF.Article

EXPERIMENTAL INVESTIGATIONS ON THE VIBRATION OF BLADES DUE TO A ROTATING STALLISHIHARA K; FUNAKAWA M.1980; BULL. ISME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 177; PP. 353-360; BIBL. 8 REF.Article

EXPERIMENTAL STUDY ON FLOW IN A SUPERSONIC CENTRIFUGAL IMPELLERSENOO Y; HAYAMI H; KINOSHITA Y et al.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 1; PP. 32-41; BIBL. 14 REF.Article

GROWTH OF A PERTURBATION IN AN AXIAL FLOW COMPRESSORFABRI J.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 1; PP. 87-94; BIBL. 13 REF.Article

DESIGN CONSIDERATIONS DURING THE ERECTION OF CABLE STAYED STEEL BRIDGES.DAS RS.1976; J. INSTIT. ENGRS (INDIA), CIV. ENGNG DIV.; INDIA; DA. 1976; VOL. 57; NO 1; PP. 61-65; BIBL. 15 REF.Article

TURBO-COMPRESSORS SURGE AND SURGE CONTROLMOBARAK A; ELARABY M; SHASH Y et al.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 9 P.; BIBL. 13 REF.Conference Paper

A BLOCKAGE MODEL FOR CENTRIFUGAL COMPRESSOR IMPELLERSPAMPREEN RC.1981; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1981; VOL. 103; NO 4; PP. 698-707; BIBL. 40 REF.Article

THE MEASUREMENT AND INTERPRETATION OF FLOW WITHIN ROTATING STALL OR CELLS IN AXIAL COMPRESSORS.DAY IJ; CUMPSTY NA.1978; J. MECH. ENGNG SCI.; GBR; DA. 1978; VOL. 20; NO 2; PP. 101-114; BIBL. 14 REF.Article

THEORETICAL STUDY OF FLOW INSTABILITIES AND INLET DISTORTIONS IN AXIAL COMPRESSORSFERRAND P; CHAUVIN J.1982; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1982; VOL. 104; NO 3; PP. 715-721; BIBL. 10 REF.Article

ETUDE DES INSTABILITES D'ECOULEMENT DANS LES SOUPAPES DE REGLAGE DE TURBINES A VAPEURPLUVIOSE M.1981; RFM, REV. FRANC. MEC.; ISSN 0373-6601; FRA; DA. 1981; NO 78; PP. 13-29; ABS. ENG; BIBL. 6 REF.Article

STALL FLUTTER OF LINEAR CASCADE IN COMPRESSIBLE FLOWKAJI S.1980; VIBRATIONS IN ROTATING MACHINERY. INTERNATIONAL CONFERENCE. 2/1980/CAMBRIDGE; GBR; LONDON: MECHANICAL ENGINEERING PUBLICATIONS; DA. 1980; PP. 209-214; BIBL. 5 REF.Conference Paper

OPTICAL DETERMINATION OF ROTATING FAN BLADE DEFLECTIONS.STARGARDTER H.1977; J. ENGNG POWER; U.S.A.; DA. 1977; VOL. 99; NO 2; PP. 204-210; BIBL. 4 REF.Article

THE EFFECT OF BOUNDARY LAYER CHANGES DUE TO TRANSIENT HEAT TRANSFER ON THE PERFORMANCE OF AXIAL-FLOW AIR COMPRESSORMACCALLUM NRL; GRANT AD.1977; S.A.E. TRANS.; USA; DA. 1977 PUBL. 1978; VOL. 86; SECTION 2; PP. 1357-1364; BIBL. 17 REF.Article

ON THE DYNAMICS OF COMPRESSOR SURGE.MCQUEEN DH.1976; J. MECH. ENGNG SCI.; G.B.; DA. 1976; VOL. 18; NO 5; PP. 234-238; BIBL. 4 REF.Article

AEROELASTICITE DES AUBES DE COMPRESSEURS. ETUDE DU FLOTTEMENT DE DECROCHAGE SUBSONIQUELOISEAU H; SZECHENYI E.1981; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1981; NO 6; PP. 393-404; ABS. ENG; BIBL. 6 REF.Article

ANALYSIS AND PREVENTION OF SUSPENSION BRIDGE FLUTTER IN CONSTRUCTION = ANALYSE ET PREVENTION DU FLUTTER DE PONT SUSPENDU EN CONSTRUCTIONBRANCALEONI F; BROTTON DM.1981; EARTHQU. ENG. STRUCT. DYN.; ISSN 0375-6297; GBR; DA. 1981; VOL. 9; NO 5; PP. 489-500; BIBL. 13 REF.Article

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