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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

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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

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THE STRUCTURE OF TURBULENT BOUNDARY LAYERS ALONG MIDLY CURVED SURFACES.RAMAPRIAN BR; SHIVAPRASAD BG.1978; J. FLUID MECH.; G.B.; DA. 1978; VOL. 85; NO 2; PP. 273-303; BIBL. 1 P. 1/2Article

THEORY OF TURBULENCE IN A HOMOGENEOUS FLUID INDUCED BY AN OSCILLATING GRIDLONG RR.1978; PHYS. OF FLUIDS; USA; DA. 1978; VOL. 21; NO 10; PP. 1887-1888; BIBL. 5 REF.Article

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METHODE DE SIMILITUDE GENERALISEE DANS LES THEORIES SEMI-EMPIRIQUES DE LA COUCHE LIMITE TURBULENTELOJTSYANSKIJ LG.1976; TRUDY L.P.I., LENINGRAD; S.S.S.R.; DA. 1976; NO 352; PP. 4-9; BIBL. 4 REF.Article

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TURBULENT BOUNDARY LAYERS WITH LARGE STREAMLINE CURVATURE EFFECTS.SO RMC; MELLOR GL.1978; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1978; VOL. 29; NO 1; PP. 54-74; ABS. ALLEM.; BIBL. 1 P. 1/2Article

NOISE GENERATED BY BOUNDARY-LAYER INTERACTION WITH PERFORATED ACOUSTIC LINERS.BAUER AB; CHAPKIS RL.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 2; PP. 157-160; BIBL. 19 REF.Article

VISCOUS EFFECTS IN TUBE FLOW INITIATED BY AN EXPANSION WAVE.KWOK ON TONG; RUSSELL DA.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 12; PP. 1763-1769; BIBL. 16 REF.Article

APPLICATION OF AN ELECTROCHEMICAL METHOD TO MEASURE THE WALL SHEAR STRESS IN A TRANSPIRED TURBULENT BOUNDARY LAYER.ITO R; HIRATA Y; MIZUSHINA T et al.1977; J. CHEM. ENGNG JAP.; JAP.; DA. 1977; VOL. 10; NO 3; PP. 188-193; BIBL. 13 REF.Article

TURBULENT BOUNDARY LAYERS AS AFFECTED BY WEAK MAGNETOHYDRODYNAMIC FORCES.SAYLES RE; LESSMANN RC.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 8; PP. 1123-1124; BIBL. 5 REF.Article

THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER IN A ROTATING HELICAL CHANNEL.ANAND AK; LAKSHMINARAYANA B.1975; J. FLUIDS ENGNG; U.S.A.; DA. 1975; VOL. 97; NO 2; PP. 197-210; BIBL. 10 REF.Article

EXPERIMENTAL METHODS AND TECHNIQUES IN TURBULENT BOUNDARY LAYER RESEARCHCOMTE BELLOT G.1980; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1980; NO 271; 35 P.; BIBL. 6 P.Conference Paper

COUCHE LIMITE TURBULENTE SUR DES SURFACES PERFOREES LORS D'UNE INSUFFLATION DIRIGEEEROSHENKO VM; ZAJCHIK LI; KLIMOV AA et al.1980; PROM. TEPLOTEH.; UKR; DA. 1980; NO 5; PP. 13-18; ABS. ENG; BIBL. 8 REF.Article

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AERODYNAMIC FORCES ON A TALL BUILDING IN A TURBULENT BOUNDARY LAYER.REINHOLD TA; TIELEMAN HW; MAHER FJ et al.1978; EXPER. MECH.; USA; DA. 1978; VOL. 18; NO 6; PP. 201-207; BIBL. 9 REF.Article

MEASUREMENT OF THE ACOUSTIC IMPEDANCE OF AN ORIFICE UNDER A TURBULENT BOUNDARY LAYER.GOLDMAN AL; PANTON RL.1976; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1976; VOL. 60; NO 6; PP. 1397-1404; BIBL. 14 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