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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

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

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

EVOLUTION OF HIGH REYNOLDS NUMBER TWO-DIMENSIONAL TURBULENCE.POUQUET A; LESIEUR M; ANDRE JC et al.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 72; NO 2; PP. 305-319; BIBL. 1 P. 1/2Article

DESIGN STUDY OF BASIC MODEL FOR USE IN THE PROPOSED 8 BY 10 FT. HIGH-REYNOLDS-NUMBER TRANSONIC WIND TUNNEL (HIRT) AT ARNOLD ENGINEERING DEVELOPMENT CENTER.ALEXANDER WK; GRIFFIN SA.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 82; PP. 1-10; BIBL. 6 REF.Conference Paper

MAGNETIC FIELD GENERATION AT HIGH MAGNETIC REYNOLDS NUMBER.LEVY EH.1978; ASTROPHYS. J.; USA; DA. 1978; VOL. 220; NO 1 PART. 1; PP. 325-329; BIBL. 23 REF.Article

AN ITERATIVE METHOD FOR THE DESIGN OF SYMMETRICAL JOUKOWSKI AIRFOILS OF SPECIFIED CHORD AND MAXIMUM THICKNESS. = METHODE ITERATIVE POUR LA CONCEPTION DE PROFILS AERODYNAMIQUES DE JOUKOWSKI SYMETRIQUES DE CORDE ET D'EPAISSEUR MAXIMALE DONNEESPITONIAK JE; SHANEBROOK JR; LEMMO AC et al.1976; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1976; VOL. 10; NO 4; PP. 723-730; BIBL. 1 REF.Article

TRANSONIC LIFT AUGMENTATION OF TWO-DIMENSIONAL SUPERCRITICAL AEROFOILS BY MEANS OF AFT CAMBER, SLOT BLOWING AND JET FLAPS, IN HIGH REYNOLDS NUMBER FLOW.PEAKE DJ; BOWKER AJ; MOKRY M et al.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 19-93; BIBL. 1 P. 1/2Conference Paper

BLOCKAGE EFFECTS ON DRAG OF SHARP-EDGED BODIES.RANGA RAJU KG; VIJAYA SINGH.1976; J. INDUSTR. AERODYN.; NETHERL.; DA. 1976; VOL. 1; NO 3; PP. 301-309; BIBL. 9 REF.Article

HYBRIDTECHNIK ZUR ERZEUGUNG TRANSSONISCHER HOHER REYNOLDSZAHL. = TECHNIQUE HYBRIDE POUR LA PRODUCTION DE NOMBRES DE REYNOLDS TRANSSONIQUES ELEVESHOTTNER T.1974; Z. FLUGWISSENSCH.; DTSCH.; DA. 1974; VOL. 22; NO 12; PP. 403-416; ABS. ANGL. FR.; BIBL. 10 REF.Article

MOUVEMENT DE CIRCULATION D'UN FLUIDE DANS UNE CAVITE RECTANGULAIRE AVEC DE GRANDS ET MOYENS NOMBRES DE REYNOLDSBELOV IA; ISAEV SA.1982; PMTF, Z. PRIKL. MEH. TEH. FIZ.; ISSN 0044-4626; SUN; DA. 1982; NO 1; PP. 41-45; BIBL. 6 REF.Article

WINDKANALUNTERSUCHUNGEN AN DUENNEN SUPERKRITISCHEN PROFILEN IM HOHEN UNTERSCHALL = ETUDE EN SOUFFLERIE DES PROFILS MINCES SUPERCRITIQUES EN ECOULEMENT SUBSONIQUE ELEVEKORNER H; PUFFERT MEISSNER W.1982; FORSCHUNGSBER.-DTSCH. FORSCH.-VERSUCHSANST. LUFT-RAUMFAHRT; ISSN 0171-1342; DEU; DA. 1982; NO 6; ABS. ENG; BIBL. 26 REF.Serial Issue

ONE-EXPONENT FOR VERY HIGH-REYNOLDS-NUMBER TURBULENCE.NELKIN M; BELL TL.1978; PHYS. REV., A; U.S.A.; DA. 1978; VOL. 17; NO 1; PP. 363-369; BIBL. 16 REF.Article

EXPERIMENTAL INVESTIGATION OF HIGH REYNOLDS NUMBER COMPRESSIBLE AXISYMMETRIC TURBULENT WAKES.AVIDOR JM; SCHNEIDERMAN AM.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 485-489; BIBL. 13 REF.Article

UNIVERSAL SIMILARITY AT HIGH GRID REYNOLDS NUMBERS.SCHEDVIN J; STEGEN GR; GIBSON CH et al.1974; J. FLUIDS MECH.; G.B.; DA. 1974; VOL. 65; NO 3; PP. 561-579; BIBL. 22 REF.Article

ETUDE DE L'ECOULEMENT SUR DES CORPS RECTANGULAIRES OU TRIANGULAIRESLECJACKS Z; PANTOFLICEK J; CHOCHOLOUS J et al.1974; SBOR. VED. PRACI, VYS. SK. CHEM.-TECHNOL. PARDUBICE; CESKOSL.; DA. 1974; VOL. 31; PP. 89-104; ABS. ANGL. ALLEM.; BIBL. 12 REF.Article

SUR LA STABILITE DE L'ECOULEMENT DE COUETTE D'UN FLUIDE DU SECOND ORDREKLIMENKOV E YA; POLUYANOV LV.1974; PRIKL. MAT. MEKH.; S.S.S.R.; DA. 1974; VOL. 38; NO 5; PP. 934-937; BIBL. 5 REF.Article

L'ECHANGE DE CHALEUR ET LA RESISTANCE AERODYNAMIQUE DES FAISCEAUX DE TUBES A AILETTES DISPOSES EN QUINCONCE, DE DIFFERENTES HAUTEURS ET PAS D'AILETTES, ET A NOMBRE RE ELEVEYUDIN VF; TOKHTAROVA LS.1972; ENERGO-MASHINOSTR.; S.S.S.R.; DA. 1972; VOL. 18; NO 12; PP. 21-23; BIBL. 5 REF.Serial Issue

THE UNSTEADY DRAG ON A SPHERICAL BUBBLE AT LARGE REYNOLDS NUMBERSPHAM DAN TAM.1982; APPL. SCI. RES.; ISSN 0003-6994; NLD; DA. 1982; VOL. 38; PP. 247-254; BIBL. 8 REF.Conference Paper

AUTODETECTION D'ONDES SONORES D'AMPLITUDE FINIE, POUR DE GRANDES VALEURS DU NOMBRE DE REYNOLDSZASLAVSKIJ YU M; SUTIN AM.1977; AKUST. ZH.; S.S.S.R.; DA. 1977; VOL. 23; NO 1; PP. 145-148; BIBL. 11 REF.Article

ON THE PROBLEM OF SHAPING AN AXISYMMETRIC BODY TO OBTAIN LOW DRAG AT LARGE REYNOLDS NUMBERS.HESS JL.1976; J. SHIP RES.; U.S.A.; DA. 1976; VOL. 20; NO 1; PP. 51-60; BIBL. 15 REF.Article

FINE-SCALED HYPERSONIC WAKES AT HIGH REYNOLDS NUMBER.FOX J.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 577; PP. 1-9; BIBL. 9 REF.Conference Paper

SIMULATION DE NOMBRES DE REYNOLDS ELEVES SUR UN CYLINDRE EN SOUFFLERIE.SZECHENYI E.1974; RECH. AEROSPAT.; FR.; DA. 1974; NO 3; PP. 155-164; ABS. ANGL.; BIBL. 5 REF.Article

AN INTERMITTENT HIGH-REYNOLDS NUMBER WIND TUNNEL.STOLLERY JL; MURTHY AV.1977; AERONAUT. QUART.; G.B.; DA. 1977; VOL. 28; NO 4; PP. 259-264; BIBL. 4 REF.Article

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