kw.\*:("NOMBRE REYNOLDS")
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THE INFLUENCE OF REYNOLDS NUMBER ON THE PERFORMANCE OF LOW MACH NUMBER, RADIAL OPEN IMPELLER.FISCHER U; ILBERG H.1973; ISRAEL J. TECHNOL.; ISRAEL; DA. 1973; VOL. 11; NO 6; PP. 373-384; BIBL. 21 REF.Article
AMORCAGE PARAMETRIQUE D'ONDES DE SURFACE MAGNETOHYDRODYNAMIQUESBRISKMAN VA; BUSKIN LN; NEVOLIN VG et al.1975; IN: 8. RIZH. SOVESHCH. MAGN. GIDRODIN. TEZISY DOKL.; RIGA; (1975); RIGA; ZINATNE; DA. 1975; VOL. 1; PP. 45-47; BIBL. 4 REF.Conference Paper
CONVECTION MIXTE DANS DES COUCHES LIMITES MAGNETOHYDRODYNAMIQUESZHIVOV MZ; SOKOVISHIN YU A.1975; IN: 8. RIZH. SOVESHCH. MAGN. GIDRODIN. TEZISY DOKL.; RIGA; (1975); RIGA; ZINATNE; DA. 1975; VOL. 1; PP. 53-55; BIBL. 2 REF.Conference Paper
THE CHARACTERISTICS OF THE PLANNED NATIONAL TRANSONIC FACILITY.MCKINNEY LW; HOWELL RR.1976; IN: AERODYN. TEST. CONF. 9. PROC.; ARLINGTON, TEX.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 176-184; BIBL. 18 REF.Conference Paper
THOUGHTS ON THE RELATIONSHIP BETWEEN REYNOLDS AND STROUHAL NUMBERS.LENHARTH W; CORELL RW.1974; J. SOUND VIBRAT.; G.B.; DA. 1974; VOL. 36; NO 1; PP. 147-149; BIBL. 17 REF.Article
UNSTEADY MAGNETOHYDRODYNAMIC FLOW IN A RECTANGULAR CHANNEL UNDER TRANSVERSE MAGNETIC FIELD.GUPTA SC; BANI SINGH.1972; INDIAN J. PURE APPL. MATH.; INDIA; DA. 1972; VOL. 3; NO 6; PP. 1038-1047; BIBL. 8 REF.Article
WALL COOLING EFFECTS ON HYPERSONIC TRANSITIONAL/TURBULENT BOUNDARY LAYERS AT HIGH REYNOLDS NUMBERS.WATSON RD.1975; IN: ANN. INST. AERONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 834; PP. 1-11; BIBL. 1 P. 1/2Conference Paper
LE CHAMP MAGNETIQUE DANS L'ECOULEMENT STATIONNAIRE AVEC EXTENSION DANS L'ESPACE DE RIEMANNARNOL'D VI; ZEL'DOVICH YA B; RUZMAJKIN AA et al.1981; Z. EKSP. TEOR. FIZ.; ISSN 0044-4510; SUN; DA. 1981; VOL. 81; NO 6; PP. 2052-2058; BIBL. 8 REF.Article
PERTURBATION D'UN CHAMP MAGNETIQUE PAR DES ECOULEMENTS DE JETS TURBULENTS D'UN LIQUIDE FAIBLEMENT CONDUCTEURFIDELIS VV.1981; MAGN. GIDRODIN.; ISSN 0025-0015; SUN; DA. 1981; NO 4; PP. 127-129; BIBL. 3 REF.Article
ETUDE DU TRANSFERT DE CHALEUR DANS LE CAS D'UN ECOULEMENT DE LIQUIDE DANS UN TUBE CIRCULAIRE, EN REGIME DE TRANSITION ET EN REGIME TURBULENT AVEC DE PETITS NOMBRES DE REYNOLDSPOPOV VN; BELYAEV VM.1975; TEPLOFIZ. VYS. TEMPER.; S.S.S.R.; DA. 1975; VOL. 13; NO 2; PP. 370-378; BIBL. 23 REF.Article
RESISTANCE HYDRAULIQUE DE LA PARTIE D'ECOULEMENT DES MACHINES MHD CYLINDRIQUESBARANOV GA; BOGDANOV YU V; BORISOV AV et al.1975; MAGNIT. GIDRODINAM., LATV. S.S.R.; S.S.S.R.; DA. 1975; NO 2; PP. 95-101; BIBL. 9 REF.Article
ENTWICKLUNG UND WINDKANALERPROBUNG VON DREI UEBERKRITISCHEN TRAGFLUEGELPROFILEN FUER VERKEHRSFLUGZEUGE. = DEVELOPPEMENT ET EXPLORATION EN SOUFFLERIE DE TROIS PROFILS D'AILES SUPERCRITIQUES POUR AVIONS DE TRANSPORTSTANEWSKY E; ZIMMER H.1975; Z. FLUGWISSENSCH.; DTSCH.; DA. 1975; VOL. 23; NO 7-8; PP. 246-256; ABS. ANGL. FR.; BIBL. 14 REF.Article
REYNOLDS NUMBER EFFECT ON AFTERBODY, THROTTLE-DEPENDENT PRESSURE FORCES.FANNING AE; GLIDEWELL RJ.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1295; PP. 1-10; BIBL. 10 REF.Conference Paper
CONSIDERATIONS FOR THE DESIGN OF A SECOND GENERATION INDUCTION DRIVEN TRANSONIC WIND TUNNEL.BRAHA J; SALOMON M; SEGINER A et al.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 12; PP. 729-735; BIBL. 17 REF.Article
A STATE-OF-THE ART SURVEY OF TWO-DIMENSIONAL AIRFOIL DATA.PROUTY RW.1975; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1975; VOL. 20; NO 4; PP. 14-25; BIBL. 32 REF.Article
PERFORMANCE CHARACTERISTICS OF AN 8-IN-DIA ASME NOZZLE OPERATING AT COMPRESSIBLE AND INCOMPRESSIBLE CONDITIONS.SMITH RE JR; MATZ RJ.1973; J. FLUIDS ENGNG; U.S.A.; DA. 1973; VOL. 95; NO 4; PP. 542-550; BIBL. 10 REF.Article
QUELQUES RESULTATS DE L'ETUDE EXPERIMENTALE DES AUBAGES PLANS D'UN PROFIL DONNE FONCTIONNANT AU GAZ NATUREL POUR DES RE DE VALEUR ELEVEEYAZIK AV; BAZ VI.1975; ENERGO-MASHINOSTR.; S.S.S.R.; DA. 1975; NO 5; PP. 43-44; BIBL. 3 REF.Article
METHOD FOR PRODUCING A UNIFORM, LOW REYNOLDS NUMBER JET.GREENE GC; BRINK DF.1974; J. SPACECR. ROCK.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 604-605; BIBL. 4 REF.Article
ON THE MHD-INSTABILITY OF SLOWLY SPREADING JETSPLASCHKO P.1980; Z. ANGEW. MATH. MECH.; DDR; DA. 1980; VOL. 60; NO 3; PP. 161-166; ABS. GER/RUS; BIBL. 14 REF.Article
VORTEX SHEDDING FROM CYLINDERS AT LOW REYNOLDS NUMBERSFRIEHE CA.1980; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1980; VOL. 100; NO 2; PP. 237-241; BIBL. 12 REF.Article
MOTION OF A CONTAMINATED DROP AT LOW REYNOLDS NUMBERSLIEYAMA K; HATANAKA JI.1976; J. CHEM. ENGNG JAP.; JAP.; DA. 1976; VOL. 9; NO 1; PP. 17-22; BIBL. 7 REF.Article
VISCOUS INCOMPRESSIBLE FLOW BETWEEN CONCENTRIC ROTATING SPHERES. III. LINEAR STABILITY AND EXPERIMENTS.MUNSON BR; MENGUTURK M.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 69; NO 4; PP. 705-719; H.T. 2; BIBL. 16 REF.Article
FORCED-CONVECTION HEAT-TRANSFER FROM A UNIFORMELY HEATED CYLINDER AT A RELATIVELY LOW REYNOLDS NUMBERS. = TRANSFERT DE CHALEUR EN CONVECTION FORCEE A PARTIR D'UN CYLINDRE UNIFORMEMENT CHAUFFE AUX NOMBRES DE REYNOLDS RELATIVEMENT FAIBLESHATTORI N.1976; BULL. J.S.M.E.; JAP.; DA. 1976; VOL. 19; NO 130; PP. 426-430; BIBL. 8 REF.Article
STABILITE DES ECOULEMENTS MAGNETOHYDRODYNAMIQUES DANS UN CANAL EN PRESENCE D'UN CHAMP EXTERIEUR OBLIQUELIKHACHEV OA; SHTERN VN.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 2; PP. 3-7; BIBL. 7 REF.Article
SULL'IMPIEGO DI ANEMOMENTO A FILO CALDO PER LA MISURO DI BASSE VELOCITA. = EMPLOI D'UN ANEMOMETRE A FIL CHAUD POUR LA MESURE DES FAIBLES VITESSESBONDI P; RUSCICA G.1974; TERMOTECNICA; ITAL.; DA. 1974; VOL. 28; NO 6; PP. 294-298; ABS. ANGL.; BIBL. 10 REF.Article