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kw.\*:("INLET FLOW")

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A FLOW STUDY IN RADIAL INFLOW TURBINE SCROLL-NOZZLE ASSEMBLY.HAMED A; BASKHARONE E; TABAKOFF W et al.1978; J. FLUIDS ENGNG; U.S.A.; DA. 1978; VOL. 100; NO 1; PP. 31-36; BIBL. 21 REF.Article

GRENZSCHICHTENTWICKLUNG BEI INSTATIONAERER ZUSTROEMUNG = DEVELOPPEMENT DES COUCHES LIMITES DANS UN ECOULEMENT D'ENTREE INSTATIONNAIREPFEIL H; HERBST R.1980; V.D.I. BER.; DEU; DA. 1980; NO 361; PP. 45-48; BIBL. 2 REF.Conference Paper

COEFFICIENT DE REMPLISSAGE DES OUVERTURES DANS LE ROTOR D'UNE SIRENE DYNAMIQUEYUDAEV VF.1979; IZVEST. VYSSH. UCHEBN. ZAVED., MASH.-STR.; SUN; DA. 1979; NO 4; PP. 96-100; BIBL. 2 REF.Article

DRUCKVER LEISTBEIWERTE VON STOSSDIFFUSOREN = COEFFICIENTS DE CHUTE DE PRESSION POUR DIFUSEURS A CHOCSREGENSCHEIT B.1979; H.L.H.; DEU; DA. 1979; VOL. 30; NO 9; PP. 319-324; ABS. ENG; BIBL. 6 REF.Article

INFLUENCE DES OSCILLATIONS DU LIQUIDE DANS LE CIRCUIT D'ALIMENTATION SUR LA PRESSION DE CHARGE D'UNE POMPE FONCTIONNANT EN REGIME AVEC DES COURANTS INVERSESKINELEV VG.1978; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1978; VOL. 21; NO 3; PP. 54-57; BIBL. 4 REF.Article

INFLUENCE DES ELEMENTS DE LA CONSTRUCTION DE LA PARTIE A ECOULEMENT SUR LA DISTRIBUTION DES PARAMETRES DERRIERE L'APPAREIL DIRECTEURGOLOSHCHAPOV VN; GRECHANICHENKO YU V.1979; TEPLOENERGETIKA (MOSK., 1954); ISSN 0040-3636; SUN; DA. 1979; NO 10; PP. 53-57; BIBL. 6 REF.Article

DIE STOSSKONFIGURATIONEN BEI STRECKENGITTERN = LA CONFIGURATION CHOC POUR DES GRILLES D'ENTREETEIPEL I.1978; Z. ANGEW. MATH. MECH.; DDR; DA. 1978; VOL. 58; NO 7; PP. 342-343Article

PREVENTION OF VORTICES AT PUMP INTAKESRAJAGOPAL HY.1981; POWER ENG. (BARRINGT., ILL.); ISSN 0032-5961; USA; DA. 1981; VOL. 85; NO 1; PP. 52-55; BIBL. 4 REF.Article

ENTRANCE CORRECTION FOR CREEPING FLOW IN SHORT TUBES.LINEHAN JH; HIRSCH SR.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 4; PP. 778-779; BIBL. 5 REF.Article

INFLUENCE OF INLET FLOW CONDITIONS AND GEOMETRIES OF CENTRIFUGAL VANELESS DIFFUSERS ON CRITICAL FLOW ANGLE FOR REVERSE FLOW.SENOO Y; KINOSHITA Y; RODGERS C et al.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 1; PP. 98-103; BIBL. 4 REF.Article

A PREDICTION METHOD FOR PLANAR DIFFUSER FLOWSBARDINA J; LYRIO A; KLINE SJ et al.1981; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1981; VOL. 103; NO 2; PP. 315-321; BIBL. 24 REF.Article

VARIATION OF FAN TONE STEADINESS FOR SEVERAL INFLOW CONDITIONSBALOMBIN JR.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMICS CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1119; 11 P.; BIBL. 11 REF.Conference Paper

INFLUENCE OF INLET FLOW CONDITIONS AND GEOMETRIES OF CENTRIFUGAL VANELESS DIFFUSERS ON CRITICAL FLOW ANGLE FOR REVERSE FLOW.SENOO Y; KINOSHITA Y.1976; IN: CENTRIFUGAL COMPRESSOR PUMP STAB. STALL SURGE. CONF.; NEW ORLEANS; 1976; NEW YORK; AM. SOC. MECH. ENG.; DA. 1976; PP. 157-166; BIBL. 4 REF.Conference Paper

UBER EIN BERECHNUNGSVERFAHREN DER VERLUSTHOEHE BEIM EINTRITTSWIDERSTAND DES WASSERS IN DIE DRAINROHRE = UN PROCEDE DE CALCUL DE LA HAUTEUR DE PERTE DE CHARGE DUE A LA RESISTANCE A LA PENETRATION DE L'EAU DANS LE TUBE DE DRAINAGEDAVID I.1983; REVUE ROUMAINE DES SCIENCES TECHNIQUES. SERIE DE MECANIQUE APPLIQUEE; ISSN 0035-4074; ROM; DA. 1983; VOL. 28; NO 1; PP. 3-20; BIBL. 17 REF.Article

ETUDE PAR UNE METHODE DE BICARACTERISTIQUES, DE L'ECOULEMENT TRIDIMENSIONNEL EN AMONT DE ROTORS DE COMPRESSEURS SUPERSONIQUESMARTINON J.1981; J. MEC. APPL.; ISSN 0399-0842; FRA; DA. 1981; VOL. 5; NO 3; PP. 323-343; ABS. ENG; BIBL. 10 REF.Article

CALCUL DE LA PARTIE INITIALE HYDRODYNAMIQUE DANS UN CANAL PLAN AVEC UTILISATION DE DIFFERENTS MODELES DE TURBULENCESHCHERBININ VI; SHKLYAR FR.1980; TEPLOFIZ. VYS. TEMP.; ISSN 0040-3644; SUN; DA. 1980; VOL. 18; NO 5; PP. 1026-1031; BIBL. 12 REF.Article

DIFFUSERS FOR SUPERSONIC INTAKES. THE DEPENDENCE OF CONICAL DIFFUSER PERFORMANCE ON INLET FLOW CONDITIONSKAMAL WA; LIVESEY JL.1979; INTERNATIONAL SYMPOSIUM ON AIR BREATHING ENGINES. 4/1979/ORLANDO FL; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1979; PP. 219-226; BIBL. 9 REF.Conference Paper

EXPERIMENTAL INVESTIGATION OF THE ORIGIN OF RESIDUAL DISTURBANCES IN TURBULENT MHD FLOWS AFTER LAMINARIZATIONBRANOVER H; GERSHON P.1979; J. FLUID MECH.; GBR; DA. 1979; VOL. 94; NO 4; PP. 629-647; BIBL. 35 REF.Article

NUMERICAL SOLUTION OF THREE-DIMENSIONAL ENTRANCE FLOW OF A BINGHAM MATERIAL THROUGH NONCIRCULAR DUCTSBATRA RL; KOSHY K.1979; COMPUTER METHODS APPL. MECH. ENGNG; NLD; DA. 1979; VOL. 19; NO 3; PP. 313-332; BIBL. 19 REF.Article

PROPAGATION OF INLET FLOW DISTORTIONS THROUGH AN AXIAL COMPRESSOR STAGECOLPIN J.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 1; PP. 116-124; BIBL. 10 REF.Article

A 2ND ORDER NUMERICAL METHOD FOR LAMINAR FLOW AT MODERATE TO HIGH REYNOLDS NUMBERS: ENTRANCE FLOW IN A DUCT.STEELE NC; BARRETT KE.1978; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1978; VOL. 12; NO 3; PP. 405-414; BIBL. 19 REF.Article

SIMULTANEOUS DEVELOPMENT OF MOMENTUM AND THERMAL BOUNDARY LAYERS IN A SUDDENLY STARTED VISCO-ELASTIC FLUID IN THE ENTRANCE REGION OF A CIRCULAR PIPE.TANDON PN; POKHARIYAL SC.1977; INDIAN J. THEOR. PHYS.; INDIA; DA. 1977; VOL. 25; NO 3; PP. 85-96; BIBL. 10 REF.Article

THE ANALYSIS OF THE ENTRANCE FLOW INTO A SLIT. I.PHILIPPOFF W.1976; TRANS. SOC. RHEOL.; U.S.A.; DA. 1976; VOL. 20; NO 3; PP. 423-439; BIBL. 15 REF.Article

STUDY OF CRITICAL GEOMETRY TWO-DIMENSIONAL DIFFUSERS HAVING DISTORTED INLET FLOWKACHHARA NL; SAXENA GB.1982; J. INST. ENG., INDIA, MECH. ENG. DIV.; ISSN 0020-3408; IND; DA. 1982; VOL. 62; NO 5; PP. 149-153; BIBL. 3 REF.Article

NONPARALLEL EFFECTS ON THE STABILITY OF DEVELOPING FLOW IN A CHANNELGARG VK; GUPTA SC.1981; PHYS. FLUIDS.; ISSN 0031-9171; USA; DA. 1981; VOL. 24; NO 9; PP. 1752-1754; BIBL. 7 REF.Article

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