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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

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

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

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

DYNAMIC INSTABILITY CAUSED BY FOREBODY BLOWINGERICSSON LE; GUENTHER RA.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 2; PP. 231-233; BIBL. 15 REF.Serial Issue

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

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

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

ROTATING STALL UND EINLAUFSTOERUNGEN IN AXIALVERDICHTERN. ZUSAMMENFASSENDE DARSTELLUNG NEUER NUMERISCHER THEORIEN = DECOLLEMENT TOURNANT ET PERTURBATIONS A L'ENTREE DANS LES COMPRESSEURS AXIAUX. RECAPITULATION DES NOUVELLES THEORIES NUMERIQUESGRAHL K; NEUHOFF HG.1981; FORSCH. INGENIEURWES.; ISSN 0015-7899; DEU; DA. 1981; VOL. 47; NO 3; PP. 69-82; ABS. ENG; BIBL. 25 REF.Article

TESTS OF AN IMPROVED ROTATING STALL CONTROL SYSTEM ON A J-85 TURBOJET ENGINELUDWIG GR; NENNI JP.1980; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1980; VOL. 102; NO 4; PP. 903-911; BIBL. 4 REF.Article

EXPERIMENTAL INVESTIGATION OF UNSTEADY PHENOMENA IN VANELESS RADIAL DIFFUSERSABDELHAMID AN; COLWILL WH; BARROWS JF et al.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 1; PP. 52-60; BIBL. 10 REF.Article

EXPERIMENTAL INVESTIGATION OF FLUTTER IN MIDSTAGE COMPRESSOR DESIGNSJUTRAS RR; STALLONE MJ; BANKHEAD HR et al.1981; J. AICR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 10; PP. 874-880; BIBL. 3 REF.Article

TORQUEWHIRL A A THEORY TO EXPLAIN NONSYNCHRONOUS WHIRLING FAILURES OF ROTORS WITH HIGH-LOAD TORQUE.VANCE JM.1978; J. ENGNG POWER; USA; DA. 1978; VOL. 100; NO 2; PP. 235-240; BIBL. 10 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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