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Results 1 to 25 of 2011

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RECHERCHE EXPERIMENTALE D'INVERSION DE CONVECTION DANS LA SOUS-COUCHE D'UNE COUCHE LIMITE TURBULENTE VISQUEUSE AVEC INJECTION DE CO2 A TRAVERS UNE SURFACE VERTICALE POREUSE CHAUFFEE A CONVECTION LIBREMOLCHADSKIJ IS.1973; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1973; VOL. 24; NO 3; PP. 440-444; ABS. ANGL.; BIBL. 3 REF.Serial Issue

SUPPRESSION OF BACKGROUND NOISE IN A TRANSONIC WIND-TUNNEL TEST SECTION. = SUPPRESSION DU BRUIT DE FOND DANS UNE SECTION D'ESSAI DE SOUFFLERIE TRANSSONIQUESCHUTZENHOFER LA; HOWARD PW.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 11; PP. 1467-1471; BIBL. 16 REF.Article

A TURBULENT BOUNDARY LAYER ANALYSIS OF CONICAL DIFFUSERS.KENNY DP.1974; C.A.S.I. TRANS., OTTAWA; CANADA; DA. 1974; VOL. 7; NO 2; PP. 49-59; BIBL. 10 REF.Article

SPECTRAL BROADENING EFFECTS IN OPEN WIND TUNNELS IN RELATION TO NOISE ASSESSMENTROSS R.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 5; PP. 567-572; BIBL. 9 REF.Article

AN INTEGRAL METHOD FOR PREDICTING BEHAVIORS OF THREE-DIMENSIONAL TURBULENT BOUNDARY LAYERS ON SHIP HULL SURFACES.HIMENO Y; TANAKA I.1974; TECHNOL. REP. OSAKA UNIV.; JAP.; DA. 1974; VOL. 23; NO 1146; PP. 617-647; BIBL. 22 REF.Article

AIRCRAFT EXCRESCENCE DRAGYOUNG AD; PATERSON JH; LLOYD JONES J et al.1981; ; FRA; DA. 1981; AGARD/AG-264; 159 P.; 30 CM; BIBL. DISSEM.; ISBN 92-835-1392-4Report

TURBULENTE SCHERSTROEMUNGEN. = ECOULEMENTS TURBULENTS CISAILLESSZABLEWSKI W.1976; SCHR.-REIHE ZENTRALINST. MATH. MECH. AKAD. WISSENSCH. D.D.R.; DTSCH.; DA. 1976; NO 21; PP. (207P.); BIBL. 3 P.Serial Issue

STRUCTURE OF TURBULENCE IN BOUNDARY LAYERS.WILLMARCH WW.1975; ADV. APPL. MECH.; U.S.A.; DA. 1975; VOL. 15; PP. 159-254; BIBL. 5 P. 1/2Article

THE TORQUE AND TURBULENT BOUNDARY LAYER OF ROTATING DISKS WITH SMOOTH AND ROUGH SURFACES, AND IN DRAG-REDUCING POLYMER SOLUTIONS.GRANVILLE PS.1973; J. SHIP RES.; U.S.A.; DA. 1973; VOL. 17; NO 4; PP. 181-195; BIBL. 24 REF.Article

TURBULENCE IN LIQUIDS. PROCEEDINGS OF THE 3RD SYMPOSIUM ON TURBULENCE IN LIQUIDS, ROLLA, MO.; 1973.1973; ; S.L.; DA. 1973; PP. (422P.); BIBL. DISSEM.Conference Proceedings

FLUID FLOW AND HEAT TRANSFER FROM ROTATING DISCSMURTHY VND.1972; MECH. CHEM. ENGNG TRANS.; AUSTRAL.; DA. 1972; VOL. 8; NO 1; PP. 48-54; BIBL. 26 REF.Serial Issue

STUDY ON A TURBULENT BOUNDARY LAYER WITH INJECTION. TURBULENT SCALESSENDA M; KAWAGUCHI Y; SUZUKI K et al.1981; BULL. JSME; ISSN 0021-3764; JPN; DA. 1981; VOL. 24; NO 196; PP. 1748-1755; BIBL. 27 REF.Article

INFLUENCE OF FREESTREAM TURBULENCE ON BOUNDARY-LAYER DEVELOPMENTMEIER HU; KREPLIN HP.1980; A.I.A.A. J. NEW YORK; USA; DA. 1980; VOL. 18; NO 1; PP. 11-15; BIBL. 8 REF.Article

TURBULENT BOUNDARY LAYERS WITH WALL INJECTION.ANTONIA RA; BECK RE.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 7; PP. 952-954; BIBL. 15 REF.Article

ZUR GLEICHUNG DER TURBULENTEN SCHUBSPANNUNG. = SUR LES EQUATIONS POUR LES CONTRAINTES TURBULENTESSZABLEWSKI W.1975; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1975; VOL. 55; NO 3; PP. 187-188; BIBL. 2 REF.Article

CANCELLATION OF TURBULENT BOUNDARY-LAYER PRESSURE FLUCTUATIONS.KENNEDY RM.1975; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1975; VOL. 57; NO 5; PP. 1062-1066; BIBL. 10 REF.Article

INVESTIGATION OF THE INSTANTANEOUS STRUCTURE OF THE WALL PRESSURE UNDER A TURBULENT BOUNDARY LAYER FLOW.EMMERLING R; MEIER GEA; DINKELACKER A et al.1974; A.G.A.R.D. CONF. PROC.; FR.; DA. 1974; NO 131; PP. 24.1-24.12; BIBL. 23 REF.; (FLUID DYN. PANEL SPEC. MEET.; BRUSSELS; 1973)Conference Paper

SOME COMMENTS ON TURBULENT BOUNDARY LAYER STRUCTURE INFERRED FROM THE MOVEMENTS OF A PASSIVE CONTAMINANT.FALCO RE.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 99; PP. 1-5; BIBL. 5 REF.Conference Paper

CARACTERISTIQUE DE LA DECOMPOSITION DES SPECTRES TURBULENTS DES FLUCTUATIONS DE PRESSIONVISHNYAKOV AA.1974; GIDROMEKHANIKA, U.S.S.R.; S.S.S.R.; DA. 1974; NO 30; PP. 22-27; BIBL. 6 REF.Article

RIBLETS AS A VISCOUS DRAG REDUCTION TECHNIQUEWALSH MJ.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 4; PP. 485-486; BIBL. 4 REF.Article

COMMENTS ON "LARGE STRUCTURE IN A TURBULENT BOUNDARY LAYER"FALCO RE.1979; PHYS. OF FLUIDS; USA; DA. 1979; VOL. 22; NO 10; PP. 2042; BIBL. 6 REF.Article

NOISE DUE TO INTERACTION OF BOUNDARY-LAYER TURBULENCE WITH A COMPRESSOR ROTOR.MOISEEV N; LAKSHMINARAYANA B; THOMPSON DE et al.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 1; PP. 53-61; BIBL. 7 REF.Article

ETUDE EXPERIMENTALE DU DECOLLEMENT DE LA COUCHE LIMITE TURBULENTE AU VOISINAGE D'UNE MARCHEDEM'YANENKO VS; ZHELTOVODOV AA.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 5; PP. 73-80; BIBL. 13 REF.Article

UNE SOLUTION INVARIANTE DE L'EQUATION DE LA COUCHE-LIMITE TURBULENTESAVEL'EV YU P.1975; P.M.T.F.; S.S.S.R.; DA. 1975; NO 4; PP. 126-132; BIBL. 10 REF.Article

"BURSTING" FREQUENCIES OBTAINED FROM WALL SHEAR STRESS FLUCTUATIONS IN A TURBULENT BOUNDARY LAYER.STRICKLAND JH; SIMPSON RL.1975; PHYS. OF FLUIDS; U.S.A.; DA. 1975; VOL. 18; NO 3; PP. 306-308; BIBL. 10 REF.Article

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