ETUDE EXPERIMENTALE DE L'INFLUENCE DES GRANDS ALLONGEMENTS DES AUBAGES SUR LES CARACTERISTIQUES AERODYNAMIQUES DES ETAGES D'UN COMPRESSEUR AXIALANYUTIN AN; ERSHOV VN; KOMLEV VI et al.1975; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1975; VOL. 18; NO 1; PP. 5-9; BIBL. 6 REF.Article

18:1 PRESSURE RATIO AXIAL/CENTRIFUGAL COMPRESSOR DEMONSTRATION PROGRAMSCHWEITZER JK; FAIRBANKS JW.1983; JOURNAL OF AIRCRAFT; ISSN 0021-8669; USA; DA. 1983; VOL. 20; NO 5; PP. 404-410; BIBL. 4 REF.Conference Paper

STABILITY OF AN AXIAL FLOW COMPRESSOR WITH STEADY INLET CONDITIONS.CORBETT AG; ELDER RL.1974; J. MECH. ENGNG SCI.; G.B.; DA. 1974; VOL. 16; NO 6; PP. 377-385; BIBL. 8 REF.Article

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

A FINITE ELEMENT METHOD FOR THE AXISYMMETRIC FLOW COMPUTATION IN A TURBOMACHINE.HIRSCH C; WARZEE G.1976; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1976; VOL. 10; NO 1; PP. 93-113; BIBL. 18 REF.Article

A COMPUTER-AIDED DESIGN PROCEDURE FOR RADIAL AND MIXED FLOW COMPRESSORS.WALLACE FJ; WHITFIELD A; ATKEY R et al.1975; COMPUTER AIDED DESIGN; G.B.; DA. 1975; VOL. 7; NO 3; PP. 163-170; BIBL. 8 REF.Article

THE CHORD-WISE PRESSURE DISTRIBUTION ON A ROTATING AXIAL FLOW COMPRESSOR BLADE.MOSES HL; O'BRIEN WF JR.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (12P.); BIBL. 1 P.Conference Paper

GROWTH OF A PERTURBATION IN AN AXIAL FLOW COMPRESSORFABRI J.1978; GAS TURBINE CONFERENCE/1978-04-09/LONDRES; USA; NEW YORK: ASME; DA. 1978; 8 P.; BIBL. 13 REF.Conference Paper

PROBLEME DE LA PENTE DES CARACTERISTIQUES DE PERFORMANCE D'UN COMPRESSEUR AXIALVORACEK V.1975; STROJN. CAS.; CESKOSL.; DA. 1975; VOL. 26; NO 2; PP. 142-155; ABS. RUSSE; BIBL. 4 REF.Article

DESIGN OF BLADE SECTIONS FOR AXIAL-FLOW COMPRESSORS.FRITH DA.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (14P.); BIBL. 1 P. 1/2Conference Paper

THE INFLUENCE OF VISCOUS INTERACTIONS ON THE FLOW DOWNSTREAM OF AN AXIAL COMPRESSOR STAGE.LOCKHART RC; WALKER GJ.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (15P.); BIBL. 17 REF.Conference Paper

ENGINE COMPRESSOR FACE RAKE FOR FLIGHT TEST INSTRUMENTATION F-14A/TF-30WEISS H; SCALLY CR.1972; I.S.A. TRANS.; U.S.A.; DA. 1972; VOL. 11; NO 4; PP. 376-393; BIBL. 17 REF.Serial Issue

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A TURBULENT BOUNDARY LAYER ANALYSIS OF CONICAL DIFFUSERS.KENNY DP.1974; C.A.S.I. TRANS., OTTAWA; CANADA; DA. 1974; VOL. 7; NO 2; PP. 49-59; BIBL. 10 REF.Article

CONVENTIONAL PROBES FOR THE RELATIVE FLOW MEASUREMENT IN A TURBOMACHINERY ROTOR BLADE PASSAGESITARAM N; LAKSHMINARAYANA B; RAVINDRANATH A et al.1981; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1981; VOL. 103; NO 2; PP. 406-414; BIBL. 17 REF.Conference Paper

BESCHAUFELUNGSAUSLEGUNG VIELSTUFIGER AXIALVERDICHTER = CONCEPTION DE L'AUBAGE D'UN COMPRESSEUR AXIAL MULTIETAGEGRAHL K.1981; BRENNST.-UBERME-KRAFT; ISSN 0006-9612; DEU; DA. 1981; VOL. 33; NO 2; PP. 59-61Article

THE EFFECT OF THE AXIAL VELOCITY DENSITY RATIO ON THE AERODYNAMIC COEFFICIENTS OF COMPRESSOR CASCADESSTARKE J.1981; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1981; VOL. 103; NO 1; PP. 210-219; BIBL. 32 REF.Article

THE EFFECTS OF THE END-WALL BOUNDARY LAYERS ON THE PERFORMANCE OF AN AXIAL COMPRESSORFOLTA V; CYRUS V.1979; CONFERENCE ON FLUID MACHINERY. 6/1979/BUDAPEST; HUN; BUDAPEST: AKAD. KIADO; DA. 1979; VOL. 1; PP. 404-412; BIBL. 6 REF.Conference Paper

VIBRATION SIGNATURE SURVEILLANCE OF AXIAL FLOW COMPRESSORSHARBARGER WB.1976; SOUND AND VIBR.; U.S.A.; DA. 1976; VOL. 10; NO 3; PP. 38-43; BIBL. 4REF.Article

NOUVELLES CONCEPTIONS SUR LE DEVELOPPEMENT DES COMPRESSEURSFRIBERG J.1976; MEC. MATER. ELECTR.; FR.; DA. 1976; NO 318-319; PP. 3-8; ABS. ANGL.Serial Issue

INVESTIGATION OF THE AXIAL VELOCITY DENSITY RATIO IN A HIGH TURNING CASCADE.STARKEN H; BREUGELMANS FAE; SCHIMMING P et al.1975; IN: GAS TURBINE CONF. PROD. SHOW; HOUSTON, TEX.; 1975; NEW YORK; AM. SOC. MECH. ENG.; DA. 1975; VOL. 75-GT-25; PP. 1-13; BIBL. 24 REF.Conference Paper

CALCUL DE LA LIMITE DU FLOTTEMENT DE GRILLES A PROFILS DYNAMIQUEMENT NON HOMOGENESDOVZENKO NV.1974; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1974; NO 2; PP. 143-147; BIBL. 6 REF.Article

ETUDE THEORIQUE DE L'INFLUENCE DU VRILLAGE DES AUBAGES SUR LE RENDEMENT D'UN ETAGE DE COMPRESSEUR AXIALBEKNEV VS; SHABAROV AB; SILANT'EV VD et al.1974; IZVEST. VYSSH. UCHEBN. ZAVED., MASH.-STR.; S.S.S.R.; DA. 1974; NO 5; PP. 91-95; BIBL. 7 REF.Article

VERDICHTER = COMPRESSEURSGALLUS HE.1974; BRENNST. WAERME KRAFT; DTSCH.; DA. 1974; VOL. 26; NO 4; PP. 172-180; BIBL. 6 P.Article

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