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Results 1 to 25 of 165713

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THREE-DIMENSIONAL BOUNDARY LAYERSEICHELBRENNER EA.1973; ANNU. REV. FLUID MECH.; U.S.A.; DA. 1973; VOL. 5; PP. 339-360; BIBL. 1 P.Serial Issue

SUR UNE SOLUTION DES EQUATIONS DE LA COUCHE LIMITE NON STATIONNAIRE TRIDIMENSIONNELLEVERESHCHAGINA LI.1974; VEST. LENINGRAD. UNIV.; S.S.S.R.; DA. 1974; NO 7; PP. 102-106; ABS. ANGL.; BIBL. 3 REF.Article

BOUNDARY LAYER OVER A BLUNT BODY AT HIGH INCIDENCE WITH AN OPEN-TYPE OF SEPARATION.WANG KC.1974; PROC. R. SOC. LONDON, A; G.B.; DA. 1974; VOL. 340; NO 1620; PP. 33-55; BIBL. 19 REF.Article

THREE-DIMENSIONAL TURBULENT BOUNDARY LAYERS-MONOGRAMSWAMY NVC; ASWATHA NARAYANA PA.1982; REV. ROUM. SCI. TECH., SER. MEC. APPL.; ISSN 0035-4074; ROM; DA. 1982; VOL. 27; NO 1; PP. 83-88; BIBL. 14 REF.Article

INVESTIGATION OF THE THREE-DIMENSIONAL BOUNDARY LAYER SEPARATION CRITERIA BY A MINIMUM PRINCIPLE.WARSI ZUA.1975; INTERNATION. J. ENGNG SCI.; G.B.; DA. 1975; VOL. 13; NO 2; PP. 161-171; BIBL. 10 REF.Article

THE ROLE OF THE ZONE OF DEPENDENCE CONCEPT IN THREE-DIMENSIONAL BOUNDARY-LAYER CALCULATIONS. = ROLE DU CONCEPT DE ZONE DE DEPENDANCE DANS LES CALCULS DES COUCHES LIMITES TRIDIMENSIONNELLESKITCHENS CW JR; SEDNEY R; GERBER N et al.1975; IN: COMPUT. FLUID DYN. CONF. 2. PROC.; HARTFORD, CONN.; 1975; S.L.; AIAA; DA. 1975; PP. 102-112; BIBL. 19 REF.Conference Paper

METHODE DES APPROXIMATIONS SUCCESSIVES POUR LES PROBLEMES DE LA COUCHE LIMITE LAMINAIRE TRIDIMENSIONNELLESHAKHOV NN; SHEVELEV YU D.1974; PRIKL. MAT. MEKH.; S.S.S.R.; DA. 1974; VOL. 38; NO 5; PP. 837-846; BIBL. 3 REF.Article

RESOLUTION APPROCHEE DU PROBLEME DE LA COUCHE LIMITE LAMINAIRE TRIDIMENSIONNELLE DANS UN FLUIDE INCOMPRESSIBLEBRYKINA IG; SHEVELEV YU D.1974; P.M.T.F.; S.S.S.R.; DA. 1974; NO 2; PP. 50-60; BIBL. 7 REF.Article

BOUNDARY LAYER ON FINITE WINGS AND RELATED BODIES WITH CONSIDERATION OF THE ATTACHEMENT LINE REGIONSCHWAMBORN D.1982; CONFERENCE ON NUMERICAL METHODS IN FLUID MECHANICS. 4/1981/PARIS; DEU; BRAUNSCHWEIG; WIESBADEN: F. VIEWEG; DA. 1982; PP. 291-300; BIBL. 5 REF.Conference Paper

LAMINARE GRENZSCHICHTEN IN DER NAEHE DER ANLEGELINIE AN FLUEGELN UND FLUEGELAEHNLICHEN KOERPERN MIT ANSTELLUNG = COUCHES LIMITES LAMINAIRES AU VOISINAGE DE LA LIGNE DE CONTACT SUR DES AILES ET D'AUTRES CORPS SEMBLABLES EN INCIDENCESCHWAMBORN D.1981; DTSCH. LUFT-RAUMFAHRT, FORSCHUNGSBER; ISSN 0070-4245; DEU; DA. 1981; NO 31; 157 P.; ABS. ENG; BIBL. 44 REF.Serial Issue

EQUATIONS UNIVERSELLES DE LA COUCHE LIMITE TRIDIMENSIONNELLE SUR UNE SURFACE CURVILIGNE PERMEABLEBOGDANOVA VV; KOZLOV LF; LISINSKAYA TI et al.1982; PRIKL. MEH. (KIEV); ISSN 0032-8243; UKR; DA. 1982; VOL. 18; NO 3; PP. 113-118; BIBL. 4 REF.Article

THE THREE DIMENSIONAL BOUNDARY LAYER ON A ROTATING HELICAL BLADEMORRIS PJ.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981-11; VOL. 112; PP. 283-296; BIBL. 8 REF.Article

SEMI-SIMILAR SOLUTIONS TO THE THREE-DIMENSIONAL LAMINAR BOUNDARY LAYER.WILLIAMS JC III.1975; APPL. SCI. RES.; NETHERL.; DA. 1975; VOL. 31; NO 3; PP. 161-186; BIBL. 9 REF.Article

DREIDIMENSIONALE GRENZSCHICHTBERECHNUNGEN ENTLANG SYMMETRIELINIEN AUF KOERPERN = CALCULS DE LA COUCHE LIMITE TRIDIMENSIONNELLE LE LONG DE LIGNES DE SYMETRIE SUR DES CORPSGRUNDMANN R.1981; Z. FLUGWISS. WELTRAUMFORSCH.; ISSN 0342-068X; DEU; DA. 1981; VOL. 5; NO 6; PP. 389-395; ABS. ENG; BIBL. 13 REF.Article

THREE-DIMENSIONAL LAMINAR BOUNDARY LAYER OVER A BODY OF REVOLUTION AT INCIDENCE AND WITH SEPARATION.GEISSLER W.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 2; PP. 1741-1745; BIBL. 8 REF.Article

TWO-LAYER MODEL OF TURBULENT BOUNDARY LAYERS.REEVES BL.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 7; PP. 932-939; BIBL. 26 REF.Article

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

ETUDE DE LA STABILITE DE LA COUCHE LIMITE COMPRESSIBLEZAJTSEV AA; SIVARAMAKRISHNAN MM.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 3; PP. 58-65; BIBL. 6 REF.Article

STABILITE DES ECOULEMENTS A PERIODICITE SPATIALE DU TYPE DE LA COUCHE LIMITELEVCHENKO V YA; SOLOV'EV AS.1974; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1974; NO 3; PP. 7-15; BIBL. 8 REF.Article

THE CALCULATION OF CAUCHY PRINCIPAL VALUES IN INTEGRAL EQUATIONS FOR BOUNDARY VALUE PROBLEMS OF THE PLANE AND THREE-DIMENSIONAL THEORY OF ELASTICITY. = CALCUL DES PRINCIPALES VALEURS DE CAUCHY DANS LES EQUATIONS INTEGRALES POUR LES PROBLEMES AUX VALEURS LIMITES EN THEORIE DE L'ELASTICITE PLANE ET TRIDIMENSIONNELLEHEISE U.1975; J. ELAST.; NETHERL.; DA. 1975; VOL. 5; NO 2; PP. 99-110; ABS. ALLEM.; BIBL. 15 REF.Article

REGIMES ET PROPRIETES DES ECOULEMENTS TRIDIMENSIONNELS A DECOLLEMENT, AMORCES PAR DES SAUTS OBLIQUES DE LA DENSITEZHELTOVODOV AA.1982; PMTF, Z. PRIKL. MEH. TEH. FIZ.; ISSN 0044-4626; SUN; DA. 1982; NO 3; PP. 116-123; BIBL. 16 REF.Article

ANALOGIE DES SINGULARITES DANS LES METHODES DIRECTES DE CALCUL DES COUCHES LIMITES TRIDIMENSIONNELLE STATIONNAIRE ET BIDIMENSIONNELLE INSTATIONNAIRE: ANALYSE DES MODES INVERSESCOUSTEIX J; HOUDEVILLE R.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 14.1-14.15; BIBL. 22 REF.Article

ON THE STABILIZATION OF THREE-DIMENSIONAL BOUNDARY LAYERS BY SUCTION AND COOLINGMACK LM.1980; LAMINAR-TURBULENT TRANSITION. SYMPOSIUM/1979/STUTTGART; DEU/USA; BERLIN: SPRINGER/NEW YORK: SPRINGER; DA. 1980; PP. 223-238; BIBL. 24 REF.Conference Paper

TURBULENCE MEASUREMENTS IN THE THREE-DIMENSIONAL BOUNDARY LAYER ON A YAWED FLAT PLATE AT INCIDENCE.CHANDRASEKHARA SWAMY NV; LAKSHMANA GOWDA BH; LAKSHMINATH VR et al.1978; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DTSCH.; DA. 1978; VOL. 2; NO 1; PP. 15-22; ABS. ALLEM.; BIBL. 28 REF.Article

CALCULATION OF GENERAL THREE-DIMENSIONAL TURBULENT BOUNDARY LAYERS.RASTOGI AK; RODI W.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 2; PP. 151-159; BIBL. 28 REF.Article

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