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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

THE INFLUENCE OF SIDE-WALL FRICTION ON SHEAR-STRESS DRIVEN ENTRAINMENT EXPERIMENTSKRANENBURG C.1983; JOURNAL OF HYDRAULIC RESEARCH; ISSN 0022-1686; NLD; DA. 1983; VOL. 21; NO 2; PP. 99-117; ABS. FRE; BIBL. 20 REF.Article

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INFLUENCE DU FROTTEMENT SUR LES PROPRIETES DEVIATRICES ET SUR LA PRESSION AU BORD DE FUITE D'UNE GRILLE D'AUBE BIDIMENSIONNELLERIBAUT M; NIESSNER H.1981; REV. BROWN BOVERI; ISSN 0302-2544; CHE; DA. 1981; VOL. 68; NO 5; PP. 197-203; BIBL. 10 REF.Article

DIRECT MEASUREMENTS OF SKIN FRICTION IN A TURBULENT BOUNDARY LAYER WITH A STRONG ADVERSE PRESSURE GRADIENTFREI D; THOMANN H.1980; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1980; VOL. 101; NO 1; PP. 79-95; BIBL. 13 REF.Article

EINFLUSS VON WANDRAUHIGKEIT, DRUCKGRADIENT UND WAERMESTROM AUF DIE WANDREIBUNGSMESSUNG MIT PRESTON-ROHREN = INFLUENCE DE LA RUGOSITE DE SURFACE, DU GRADIENT DE PRESSION ET DU TRANSFERT DE CHALEUR SUR LA MESURE DU FROTTEMENT SUPERFICIEL AVEC DES TUBES DE PRESTONNITSCHE W; HABERLAND C.1980; ILR-BER.; ISSN 0341-0587; DEU; DA. 1980; NO 50; 40 P.; ABS. ENG; BIBL. 20 REF.Serial Issue

ZUR KOMPRESSIBLEN REIBUNGSBEHAFTETEN STROEMUNG DURCH BESCHAUFELTE RADIALDIFFUSOREN = ECOULEMENT COMPRESSIBLE AVEC FROTTEMENT DANS LES DIFFUSEURS RADIAUX MUNIS D'AUBESBRANDT U; TEIPEL I.1980; V.D.I. BER.; DEU; DA. 1980; NO 361; PP. 273-275; BIBL. 5 REF.Conference Paper

EFFECTS OF A SHARP PRESSURE RISE ON A COMPRESSIBLE LAMINAR BOUNDARY LAYER WHEN THE PRANDTL NUMBER IS SIGMA =0,72CURLE N.1979; PROC. R. SOC. EDINBURGH, A; GBR; DA. 1979; VOL. 84; NO 1-2; PP. 153-171; BIBL. 12 REF.Article

AN INVESTIGATION OF MULTIPLE ORIFICE WALL JETSSMITH VK III; HUBBARTT JE.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-158; 11 P.; BIBL. 32 REF.Conference Paper

DE L'INFLUENCE DES PHENOMENES PHYSICO-CHIMIQUES SUR LA FRICTION SUPERFICIELLE, DANS L'ECOULEMENT HYPERSONIQUE D'UN GAZ AUTOUR D'UN CORPS OBTUSGOLOVACHEV YU P; POPOV FD.1976; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1976; VOL. 31; NO 6; PP. 1126-1128; ABS. ANGL.; BIBL. 7 REF.Article

A STUDY OF THE MOTION OF OIL FILMS ON SURFACES IN AIR FLOW, WITH APPLICATION TO THE MEASUREMENT OF SKIN FRICTION.TANNER LH; BLOWS LG.1976; J. PHYS. E; G.B.; DA. 1976; VOL. 9; NO 3; PP. 194-202; BIBL. 13 REF.Article

THE LAMINAR FLOW VELOCITY PROFILE OVER CLOSE-PACKED SPHERICAL ROUGHNESS ELEMENTSCOLEMAN NL.1982; HOUILLE BLANCHE; ISSN 0018-6368; FRA; DA. 1982; VOL. 37; NO 1; PP. 13-22; BIBL. 7 REF.; IDEM FREArticle

FLOW PATTERN AND FRICTIONAL LOSSES IN PULSATING PIPE FLOW. IV: GENERAL REPRESENTATION OF TURBULENT FRICTIONAL LOSSESOHMI M; IGUCHI M.1981; BULL. JSME; ISSN 0021-3764; JPN; DA. 1981; VOL. 24; NO 187; PP. 67-74; BIBL. 7 REF.Article

ON OSCILLATIONS IN A COMPRESSIBLE LAMINAR BOUNDARY LAYERGRIBBEN RJ.1981; PROC. R. SOC. EDINB., SECT. A, MATH.; ISSN 0308-2105; GBR; DA. 1981; VOL. 91; NO 1-2; PP. 1-13; BIBL. 5 REF.Article

DER EINFLUSS DES KAPILLARENMATERIALS AUF DIE VERRINGERUNG DES REIBUNGSWIDERSTANDES = INFLUENCE DU MATERIAU DU CAPILLAIRE SUR LA REDUCTION DE TRAINEEDSCHAGAROWA E; BOCHOSSJAN T.1980; RHEOL. ACTA; DEU; DA. 1980; VOL. 19; NO 2; PP. 258-261; ABS. ENG; BIBL. 11 REF.Article

THE FRICTIONAL CHARACTERISTICS OF ALLUVIAL STREAMS: A NEW RAPPROACHWHITE WR; PARIS E; BETTESS R et al.1980; INSTIT. CIV. ENGRS, PROC.; GBR; DA. 1980-09; VOL. 69; PART. 2; PP. 737-750; BIBL. 7 REF.Article

EFFECT OF WALL FRICTION AND VORTEX GENERATION ON THE RADIAL DISTRIBUTION OF DIFFERENT PHASES.ROUHANI Z.1976; INTERNATION. J. MULTIPHASE FLOW; G.B.; DA. 1976; VOL. 3; NO 1; PP. 35-50; BIBL. 21 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