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SUR LE TRANSFERT DE CHALEUR DANS UNE COUCHE LIMITE LAMINAIREPORICEL DINU M.1973; STUD. CERC. MAT.; ROMAN.; DA. 1973; VOL. 25; NO 1; PP. 45-51; ABS. FR.; BIBL. 1 REF.Serial Issue

MIXED CONVECTION ABOVE A HEATED HORIZONTAL SURFACEHIEBER CA.1973; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1973; VOL. 16; NO 4; PP. 769-785; ABS. FR. ALLEM. RUSSE; BIBL. 9 REF.Serial Issue

AERODYNAMIC HEATING FOR GAPS IN LAMINAR AND TRANSITIONAL BOUNDARY LAYERSBERTIN JJ; GOODRICH WD.1981; PROGR. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 77; PP. 3-35; BIBL. 14 REF.Conference Paper

COUCHE LIMITE LAMINAIRE DANS UN ECOULEMENT TOURBILLONNAIREBELYANIN NM; SHAL'MAN E YU.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 1; PP. 43-49; BIBL. 10 REF.Article

DETERMINATION DE LA TEMPERATURE DANS LA COUCHE LIMITE COMPTE TENU DU PHENOMENE DE GLISSEMENTMAKSAY S.1976; STUD. CERC. MAT.; ROMAN.; DA. 1976; VOL. 28; NO 3; PP. 283-287; ABS. FR.; BIBL. 5 REF.Article

LAMINAR BOUNDARY LAYER OVER A FLEXIBLE SURFACE IN OSCILLATORY FLOW. I. NEWTONIAN FLUID.PATHAK SK; CHATURVEDI MC.1975; PROC. INDIAN ACAD. SCI., A; INDIA; DA. 1975; VOL. 81; NO 4; PP. 164-178; BIBL. 8 REF.Article

COUCHE LIMITE LAMINAIRE ENTRE DEUX ECOULEMENTS PARALLELESJONAS P.1974; STROJN. CAS.; CESKOSL.; DA. 1974; VOL. 25; NO 6; PP. 689-698; ABS. RUSSE; BIBL. 4 REF.Article

EFFET DE LA CONDUCTION DANS LES PAROIS SUR LE TRANSFERT CHALEUR CONVECTIF AVEC COUCHE LIMITE LAMINAIRESAKAKIBARA M; MORI S; TANIMOTO A et al.1973; KAGAKU KOGAKU; JAP.; DA. 1973; VOL. 37; NO 3; PP. 281-288; ABS. ANGL; BIBL. 13 REF.Serial Issue

EFFECT OF SMALL AMPLITUDE WALL WAVINESS UPON THE STABILITY OF THE LAMINAR BOUNDARY LAYER. = EFFET D'UNE ONDULATION DE FAIBLE AMPLITUDE DE LA PAROI SUR LA COUCHE LIMITE LAMINAIRELESSEN M; GANGWANI ST.1976; PHYS. OF FLUIDS; U.S.A.; DA. 1976; VOL. 19; NO 4; PP. 510-513; BIBL. 9 REF.Article

ON LAMINAR BOUNDARY LAYERS IN OSCILLATORY FLOW.PATEL MH.1975; PROC. R. SOC. LONDON, A; G.B.; DA. 1975; VOL. 347; NO 1648; PP. 99-123; BIBL. 12 REF.Article

METHODE APPROCHEE DE CALCUL DES PARAMETRES DE LA COUCHE LIMITE LAMINAIRE DANS UN DIFFUSEURGIROL AP; KATERINA EI.1975; PRIKL. MEKH., U.S.S.R.; S.S.S.R.; DA. 1975; VOL. 11; NO 1; PP. 129-132; BIBL. 2 REF.Article

HEAT TRANSFER DURING THE FLOW OF A MEDIUM FROM THE CENTER TO THE PERIPHERY BETWEEN TWO ROTATING DISKS = TRANSFERT DE CHALEUR LORS DE L'ECOULEMENT D'UN MILIEU DU CENTRE VERS LA PERIPHERIE ENTRE DEUX DISQUES EN ROTATIONKIPINOS VM; PUSTOVALOV VN; RUD'KO AP et al.1973; HEAT TRANSFER, SOVIET RES.; U.S.A.; DA. 1973; VOL. 5; NO 1; PP. 1-9; BIBL. 5 REF.Serial Issue

HEAT TRANSFER THROUGH THE UNSTEADY LAMINAR BOUNDARY LAYER ON A SEMI-INFINITE FLAT PLATE. II. EXPERIMENTAL RESULTS FROM AN OSCILLATING PLATEEVANS NA.1973; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1973; VOL. 16; NO 3; PP. 567-580; H.T. 1; ABS. FR. ALLEM. RUSSE; BIBL. 23 REF.Serial Issue

LEAST SQUARES FINITE ELEMENT ANALYSIS OF LAMINAR BOUNDARY LAYER FLOWS.LYNN PP.1974; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1974; VOL. 8; NO 4; PP. 865-876; BIBL. 15 REF.Article

METHODE PARAMETRIQUE DE RESOLUTION GENERALE DES PROBLEMES DE COUCHE LIMITE LAMINAIRELOJTSYANSKIJ LG.1974; IN: IZBR. PROBL. PRIKL. MEKH.; MOSKVA; VINITI; DA. 1974; PP. 467-474; BIBL. 11 REF.Book Chapter

HEAT TRANSFER THROUGH THE UNSTEADY LAMINAR BOUNDARY LAYER ON A SEMI-INFINITE FLAT PLATE. I. THEORETICAL CONSIDERATIONSEVANS NA.1973; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1973; VOL. 16; NO 3; PP. 555-565; ABS. FR. ALLEM. RUSSE; BIBL. 18 REF.Serial Issue

NATURAL CONVECTION BOUNDARY LAYER FLOW OVER HORIZONTAL AND SLIGHTLY INCLINED SURFACESPERA L; GEBHART B.1973; INTERNATION. J. HEAT MASS TRANSFER; G.B.; DA. 1973; VOL. 16; NO 6; PP. 1131-1146; H.T. 1; ABS. FR. ALLEM. RUSSE; BIBL. 6 REF.Serial Issue

LAMINAR BOUNDARY-LAYER INDUCED WAVE FORCES ON A SUBMERGED FLAT-PLATE HYDROFOIL. = FORCES D'ONDES INDUITES PAR COUCHE-LIMITE LAMINAIRE SUR UN PROFIL HYDRODYNAMIQUE IMMERGE A PLAQUE PLANEPLOTKIN A.1974; J. HYDRONAUT.; U.S.A.; DA. 1974; VOL. 8; NO 2; PP. 47-53; BIBL. 27 REF.Article

ETUDE THEORIQUE DE LA COUCHE LIMITE LAMINAIRE DANS LA REGION LA MOINS EXPOSEE AU VENT D'UN CONE EN INCIDENCE.FORESTIER B.1974; AO-CNRS-11328; FR.; DA. 1974; PP. 1-66; H.T. 19; BIBL. 4 P.; (THESE DOCT.-ING.; PROVENCE)Thesis

A LAMINAR BOUNDARY LAYER ON A ROTATING THREE-DIMENSIONAL BLADE.MIYAKE Y; FUJITA S.1974; J. FLUIDS MECH.; G.B.; DA. 1974; VOL. 65; NO 3; PP. 481-498; BIBL. 7 REF.Article

UNSTEADY LAMINAR BOUNDARY LAYERS.RILEY N.1975; S.I.A.M. REV.; U.S.A.; DA. 1975; VOL. 17; NO 2; PP. 274-297; BIBL. 2 P. 1/2Article

CONSTRUCTION D'UNE SOLUTION MULTIPARAMETRIQUE DANS LE DOMAINE D'ACCELERATION BRUSQUE DE LA COUCHE LIMITE LAMINAIREELISEEV VI.1975; PRIKL. MEKH., U.S.S.R.; S.S.S.R.; DA. 1975; VOL. 11; NO 6; PP. 101-108; BIBL. 9 REF.Article

SUCCION OPTIMALE DE LA COUCHE LIMITE LAMINAIRE SUR UNE SURFACE CURVILIGNE A ISOLATION THERMIQUE DANS UN GAZ COMPRIMEKOZLOV LF; MIZYUK VG.1975; PRIKL. MEKH., U.S.S.R.; S.S.S.R.; DA. 1975; VOL. 11; NO 9; PP. 129-133; BIBL. 4 REF.Article

EFFECT OF CHANGE IN CENTRIFUGAL IMPELLER WIDTH ON BOUNDARY LAYER FLOW ALONG BLADE SURFACE.OGAWA T; MAEKAWA A; MURATA S et al.1974; TECHNOL. REP. OSAKA UNIV.; JAP.; DA. 1974; VOL. 24; NO 1191-1229; PP. 739-750; BIBL. 8 REF.Article

CERTAINS ASPECTS NOUVEAUX DE LA THEORIE DE LA COUCHE LIMITE LAMINAIRELOJTSYANSKIJ LG; STEPANYANTS LG.1974; TRUDY L.P.I., LENINGRAD; S.S.S.R.; DA. 1974; NO 339; PP. 94-101; BIBL. 14 REF.Article

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