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

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

ENTRANCE REGION HEAT TRANSFER BETWEEN PARALLEL PLATES WITH UNIFORM WALL TEMPERATURELOU YS; BARTON LO.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 393-394; BIBL. 5 REF.Serial Issue

HEAT TRANSFER FOR DEVELOPING LAMINAR FLOW IN THE ENTRANCE OF A TUBEROY DN.1968; J. INSTIT. ENGRS (INDIA), MECH. ENGNG DIV.; INDIA; DA. 1968; VOL. 49; NO 1; PP. 71-79; BIBL. 18 REF.Serial Issue

THE PRANDTL NUMBER DEPENDENCE OF THE CONVECTIVE HEAT TRANSFER COEFFICIENT IN A TURBULENT THERMAL ENTRANCE REGIONEISSENBERG DM; DAY JT; PORTAL C et al.1973; A.I. CH. E.J., NEW YORK; U.S.A.; DA. 1973; VOL. 19; NO 2; PP. 393-394; BIBL. 4 REF.Serial Issue

CARACTERISTIQUES NON LINEAIRES D'UNE AILE MINCE LORS D'UN ECOULEMENT SANS A COUPS DU BECPAVLENKO VS.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 5; PP. 183-185; BIBL. 3 REF.Article

STABILITY OF THE DEVELOPING LAMINAR PIPE FLOW.HUANG LM; CHEN TS.1974; PHYS. OF FLUIDS; U.S.A.; DA. 1974; VOL. 17; NO 1; PP. 245-247; BIBL. 16 REF.Article

TURBULENT FLOW IN THE ENTRY REGION OF A ROUGH PIPE.JENG SONG WANG; TULLIS JP.1974; J. FLUIDS ENGNG; U.S.A.; DA. 1974; VOL. 96; NO 1; PP. 62-68; BIBL. 12 REF.Article

INLET DISTORTION AND BLADE VIBRATION IN TURBOMACHINERY.TANIDA Y.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (10P.); BIBL. 8 REF.Conference Paper

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

AN INVESTIGATION INTO THERMAL BOUNDARY LAYER GROWTH IN THE ENTRANCE REGION OF AN ANNULUSSRIVASTAVA NC; BAKHTAR F; BANNISTER FK et al.1973; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1973; VOL. 16; NO 1; PP. 49-59; H.T. 1; ABS. FR. ALLEM. RUSSE; BIBL. 14 REF.Serial Issue

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

CONVECTIVE INSTABILITY IN THE THERMAL ENTRANCE REGION OF A HORIZONTAL PARALLEL-PLATE CHANNEL HEATED FROM BELOWHWANG GJ; CHENG KC.1973; J. HEAT TRANSFER; U.S.A.; DA. 1973; VOL. 95; NO 1; PP. 72-77; BIBL. 8 REF.Serial Issue

CORRELATIONS FOR LAMINAR FORCED CONVECTION WITH UNIFORM HEATING IN FLOW OVER A PLATE AND IN DEVELOPING AND FULLY DEVELOPED FLOW IN A TUBECHURCHILL SW; OZOE H.1973; J. HEAT TRANSFER; U.S.A.; DA. 1973; VOL. 95; NO 1; PP. 78-84; BIBL. 25 REF.Serial Issue

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

JOULE-THOMSON EFFECTS ON THERMAL ENTRANCE REGION HEAT TRANSFER IN PIPES WITH UNIFORM WALL TEMPERATURECHENG KC; JENN WUU OU.1973; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1973; VOL. 16; NO 3; PP. 696-699; BIBL. 6 REF.Serial Issue

EXPERIMENTAL INVESTIGATION OF A TRANSONIC AXIAL FLOW COMPRESSOR STAGE WITH STEADY STATE DISTORTED INLET FLOW.LECHT M; WEYER H.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (15P.); BIBL. 4 REF.Conference Paper

NOISE GENERATION BY STEADY AND UNSTEADY FLOW DISTORTIONS.MATHER JSB; FISHER MJ.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (15P.); BIBL. 11 REF.Conference Paper

STABILITY OF DEVELOPING FLOW IN A PIPE: NON-AXISYMMETRIC DISTURBANCESGARG JK.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981-09; VOL. 110; PP. 209-216; BIBL. 21 REF.Article

ENTRANCE FLOW OF A BINGHAM FLUID IN A TUBE.SHAH VL; SOTO RJ.1975; APPL. SCI. RES.; NETHERL.; DA. 1975; VOL. 30; NO 4; PP. 271-278; BIBL. 6 REF.Article

ENTRY FLOW IN A CURVED PIPE.YAO LS; BERGER SA.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 67; NO 1; PP. 177-196; BIBL. 17 REF.Article

INCOMPRESSIBLE TURBULENT BOUNDARY LAYER IN THE INLET REGION OF A SMOOTH PIPE.RAGHUNATHAN S; SUBIR KAR.1975; INDIAN J. TECHNOL.; INDIAN; DA. 1975; VOL. 13; NO 2; PP. 64-65; BIBL. 3 REF.Article