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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

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

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

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

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

SELECTIVE DECAY HYPOTHESIS AT HIGH MECHANICAL AND MAGNETIC REYNOLDS NUMBERSMATTHAEUS WH; MONTGOMERY D.1980; ANN. N.Y. ACAD. SCI.; ISSN 0077-8923; USA; DA. 1980; VOL. 357; PP. 203-222; BIBL. 39 REF.Conference Paper

THE USE OF ROUGHNESS TO PRODUCE HIGH REYNOLDS NUMBER FLOWS AROUND CIRCULAR CYLINDERS AT LOWER REYNOLDS NUMBERSLAWSON TV.1982; J. WIND ENG. IND. AERODYN.; ISSN 0167-6105; NLD; DA. 1982; VOL. 10; NO 3; PP. 381-387; BIBL. 2 REF.Article

HYDROMAGNETIC FLOW PAST A POROUS FLAT PLATE WITH HALL EFFECTS.GUPTA AS.1975; ACTA MECH.; AUTR.; DA. 1975; VOL. 22; NO 3-4; PP. 281-287; ABS. ALLEM.; BIBL. 8 REF.Article

THE EFFECTS OF SURFACE ROUGHNESS AND TUNNEL BLOCKAGE ON THE FLOW PAST SPHERES.ACHENBACH E.1974; J. FLUID MECH.; G.B.; DA. 1974; VOL. 65; NO 1; PP. 113-125; BIBL. 4 REF.Article

EXPERIMENTAL STUDY OF SUPERSONIC DIFFUSERS WITH LARGE ASPECT RATIOS AND LOW REYNOLDS NUMBERSKRAUSE S.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 1; PP. 94-101; BIBL. 20 REF.Article

ECOULEMENT D'UN LIQUIDE A TRAVERS DES TUYERES CYLINDRIQUES EXTERIEURES AVEC UNE ENTREE RADIALE)SKOBEL'TSYN YU A; KOMLEV AF.1976; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; S.S.S.R.; DA. 1976; VOL. 19; NO 3; PP. 109-113; BIBL. 6 REF.Article

LAMINAR SEPARATION AT A TRAILING EDGE. = DECOLLEMENT LAMINAIRE A UN BORD DE FUITEGUIRAUD JP; SCHMITT R.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 3.1-3.5; ABS. FR.; BIBL. 11 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOETTINGEN, GER.; 1975)Conference Paper

EXCITATION DE JETS A HAUTE VITESSE PAR DES VIBRATIONS ACOUSTIQUESBORISOV YU YA; GYNKINA NM.1975; AKUST. ZH.; S.S.S.R.; DA. 1975; VOL. 21; NO 3; PP. 364-371; BIBL. 10 REF.Article

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