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Results 1 to 25 of 1799

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INFLUENCE DE LA COMPOSANTE NORMALE DE LA VITESSE SUR LES PARAMETRES DE LA ZONE PARIETALE DE LA COUCHE LIMITEGIROL AP; MIKITIN YA A.1976; PRIKL. MEKH., U.S.S.R.; S.S.S.R.; DA. 1976; VOL. 12; NO 3; PP. 132-136Article

RESONATING WATERFALLS.BINNIE AM; MAYERS DF.1974; PROC. R. SOC. LONDON, A; G.B.; DA. 1974; VOL. 339; NO 1619; PP. 435-449; BIBL. 6 REF.Article

MESURES DU FROTTEMENT ET DU TRANSFERT DE CHALEUR A MACH 2 ET A NOMBRES DE REYNOLDS ELEVESHOURS Y.1974; RECH. AEROSPAT.; FR.; DA. 1974; NO 6; PP. 355-365; ABS. ANGL.; BIBL. 6 REF.Article

THE EFFECT OF SURFACE ROUGHNESS CHARACTER ON TURBULENT RE-ENTRY HEATINGFINSON ML; CLARKE AS.1981; PROG. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 77; PP. 83-108; BIBL. 17 REF.Conference Paper

COMPLIANT WALL-TURBULENT SKIN-FRICTION REDUCTION RESEARCH.FISCHER MC; WEINSTEIN LM; ASH RL et al.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 833; PP. 1-30; BIBL. 2 P.Conference Paper

UNIFIED NONLINEAR APPROACH TO BOTH WEAK AND STRONG-INTERACTION PROBLEMS.GUPTA RN; RODKIEWICZ CM.1975; ACTA MECH.; AUTR.; DA. 1975; VOL. 21; NO 1-2; PP. 53-63; ABS. ALLEM.; BIBL. 10 REF.Article

DU PROBLEME DE CONTACT PLAN EN THEORIE DU FLUAGE TENANT COMPTE DES FORCES DE FROTTEMENT, AVEC DEUX ENDROITS DE CONTACTMANUKYAN MM.1973; IZVEST. AKAD. NAUK ARM. S.S.R., MEKH.; S.S.S.R.; DA. 1973; VOL. 26; NO 5; PP. 55-74; ABS. ARM. ANGL.; BIBL. 9 REF.Article

TOTAL HEAD/STATIC MEASUREMENTS OF SKIN FRICTION AND SURFACE PRESSURE.BERTELRUD A.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 436-438; BIBL. 8 REF.Article

LOI DU FROTTEMENT ET PARAMETRES DE FORME D'UN ECOULEMENT TOURBILLONNAIRE DANS UN CANAL CYLINDRIQUEKHALATOV AA; SHCHUKIN VK; LETYAGIN VG et al.1977; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1977; NO 3; PP. 98-105; BIBL. 8 REF.Article

A MORE ACCURATE VISCOSITY BALANCE MEASUREMENT OF THE VARIATION OF SKIN FRICTION WITH REYNOLDS NUMBER FOR COMPARISON WITH PRESTON TUBES.TANNER LH.1977; J. PHYS. E; G.B.; DA. 1977; VOL. 10; NO 8; PP. 843; BIBL. 2 REF.Article

ETUDE DU MOUVEMENT INSTATIONNAIRE D'UN FLUIDE LORS DE PROCESSUS DE TRANSITION DANS UN TUBE COURTPOPOV DN; KRAVCHENKO VG.1974; VEST. MASHINOSTR.; S.S.S.R.; DA. 1974; VOL. 54; NO 6; PP. 7-10; BIBL. 4 REF.Article

NEW SKIN FRICTION AND ENTRAINMENT CORRELATIONS FOR TURBULENT BOUNDARY LAYERSFERZIGER JH; LYRIO AA; BARDINA JG et al.1982; JOURNAL OF FLUIDS ENGINEERING; ISSN 0098-2202; USA; DA. 1982; VOL. 104; NO 4; PP. 537-540; BIBL. 3 REF.Article

THE MEASUREMENT OF SKIN FRICTION IN A HIGHLY TURBULENT FLOW.PRIHODA J.1975; ARCH. BODOWY MARZ.; POLSKA; DA. 1975; VOL. 22; NO 1; PP. 35-40; ABS. POL. RUSSE; BIBL. 5 REF.Article

NOTE ON BOUNDARY LAYER IN A DUSTY GAS.CHAKRABARTI KM.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1136-1137; BIBL. 4 REF.Article

SOLUTION EN SERIES DE PUISSANCES D'ORDRE SUPERIEUR POUR UNE COUCHE LIMITE DE PLAQUE PLANE AVEC INJECTION UNIFORMEHONMA H; SATO Y.1973; J. FAC. ENGNG CHIBA UNIV.; JAP.; DA. 1973; VOL. 25; NO 47; PP. 1-4; ABS. ANGL.; BIBL. 2 REF.Article

PRESSURE RISE TO SEPARATION IN CYLINDRICALLY SYMMETRIC SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION. = HAUSSE DE LA PRESSION DU DECOLLEMENT DANS L'INTERACTION ONDE DE CHOC A SYMETRIE CYLINDRIQUE-COUCHE LIMITE TURBULENTEMYRING DF.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. (14P.); BIBL. 1 P. 1/2; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOTTINGEN, GER.; 1975)Conference Paper

INFLUENCE DU SOUFFLAGE ET DE L'ASPIRATION DU FLUIDE COMPRESSIBLE D'UN JET SEMI LIMITE SUR LE FROTTEMENT SUPERFICIELGIROL AP.1975; GIDROMEKHANIKA, U.S.S.R.; S.S.S.R.; DA. 1975; NO 30; PP. 27-30Article

UNSTEADY VISCOUS FLOW DUE TO THE IMPULSIVE MOTION OF A FLAT PLATE. II.YOSHIZAWA A.1974; J. PHYS. SOC. JAP.; JAP.; DA. 1974; VOL. 36; NO 1; PP. 271-275; BIBL. 6 REF.Article

AN EMPIRICAL DESCRIPTION OF WALL JET VELOCITY PROFILES.CHANDRASEKHARA SWAMY NV; LAKSHMANA GOWDA BH; CHANDRASHEKHAR N et al.1975; INDIAN J. TECHNOL.; INDIA; DA. 1975; VOL. 13; NO 3; PP. 103-106; BIBL. 10 REF.Article

FRICTION FACTORS IN THE THEORY OF BIFURCATING POISEUILLE FLOW THROUGH ANNULAR DUCTS.JOSEPH DD; CHEN TS.1974; J. FLUID MECH.; G.B.; DA. 1974; VOL. 66; NO 1; PP. 189-207; BIBL. 12 REF.Article

MICROSTRUCTURE DE L'ECOULEMENT TURBULENT ETABLI DANS UN CANAL BIDIMENSIONNEL AVEC UN RAPPORT DES COTES 1/9 ET DES ANGLES ARRONDISDYBAN EP; EHPIK EH YA; FILIPCHUK VE et al.1974; TEPLOFIZ. I TEPLOTEKH., U.S.S.R.; S.S.S.R.; DA. 1974; NO 26; PP. 26-29; BIBL. 5 REF.Article

SIMPLE AND EXPLICIT FORMULAS FOR THE FRICTION FACTOR IN TURBULENT PIPE FLOWHAALAND SE.1983; JOURNAL OF FLUIDS ENGINEERING; ISSN 0098-2202; USA; DA. 1983; VOL. 105; NO 1; PP. 89-90; BIBL. 8 REF.Article

RELAXATION DES CONTRAINTES DE FROTTEMENT DE REYNOLDS DANS UNE COUCHE LIMITE TURBULENTE DESEQUILIBREEZYABRIKOV VV.1983; INZENERNO-FIZICESKIJ ZURNAL; ISSN 0021-0285; BYS; DA. 1983; VOL. 44; NO 4; PP. 561-564; ABS. ENG; BIBL. 6 REF.Article

A NOTE ON EXPANSIONS FOR THE TWO-DIMENSIONAL, COMPRESSIBLE, LAMINAR BOUNDARY LAYER EQUATIONS NEAR A POINT OF ZERO SKIN FRICTIONWILKS G.1983; PROCEEDINGS OF THE ROYAL SOCIETY OF EDINBURGH. SECTION A. MATHEMATICS; ISSN 0308-2105; GBR; DA. 1983; VOL. 94; NO 1-2; PP. 93-96; BIBL. 4 REF.Article

JAUGES A FIL CHAUD POUR LA MESURE DU FROTTEMENT PARIETAL (REALISATION, ETALONNAGE, APPLICATIONS)COUSTEIX J; JUILLEN JC.1982; RECH. AEROSP.; ISSN 0034-1223; FRA; DA. 1982; NO 3; PP. 207-218; ABS. ENG; BIBL. 14 REF.Article

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