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kw.\*:("LAMINAR BOUNDARY LAYER")

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Results 1 to 25 of 1304

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QUASI-THREE-DIMENSIONAL LAMINAR BOUNDARY-LAYER SEPARATIONS IN SUPERSONIC FLOW.VATSA VN; WERLE MJ.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 4; PP. 634-639; BIBL. 28 REF.Article

DE LA RESOLUTION DES EQUATIONS DE LA COUCHE LIMITE PAR LA METHODE DES SERIES INVERSEESBASHKIN VA; DZHAMGAROV GM.1977; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1977; VOL. 20; NO 4; PP. 5-12; BIBL. 8 REF.Article

A NONASYMPTOTIC TRIPLE DECK MODEL FOR SUPERSONIC BOUNDARY-LAYER INTERACTION.KING MONG TU; WEINBAUM S.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 6; PP. 767-775; BIBL. 26 REF.Article

EXISTENZ UND EINDEUTIGKEIT DER GOERTLER-FUNKTIONEN = EXISTENCE ET UNICITE DE LA FONCTION DE GOERTLERSCHWIERZ KP.1978; Z. ANGEW. MATH. MECH.; DDR; DA. 1978; VOL. 58; NO 7; PP. 324-325; BIBL. 7 REF.Article

OPTIMAL COORDINATES FOR THREE-DIMENSIONAL INCOMPRESSIBLE LAMINAR BOUNDARY LAYERS.WARSI ZUA.1977; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1977; VOL. 28; NO 3; PP. 467-479; ABS. FR.; BIBL. 11 REF.Article

TWO-DIMENSIONAL, LAMINAR, COMPRESSIBLE BOUNDARY-LAYER CALCULATIONS IN TURBOMACHINES.GRUNDMANN R.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 7; PP. 897-898; BIBL. 4 REF.Article

THEORETICAL STUDY OF THE FLOW FIELD INSIDE A HYDROCYCLONE WITH VORTEX FINDER DIAMETER GREATER THAN THAT OF APEX OPENING. I: LAMINAR CASEBHATTACHARYYA P.1980; APPL. SCI. RES.; ISSN 0003-6994; NLD; DA. 1980; VOL. 36; NO 3; PP. 197-212; BIBL. 15 REF.Article

DECOLLEMENT D'UN ECOULEMENT LE LONG D'UNE LIGNE D'UNE SURFACE REGULIERELEGENDRE R.1978; RECH. AEROSPAT.; FRA; DA. 1978; NO 5; PP. 213-219; ABS. ENG; BIBL. 10 REF.Article

METHODE DE LA SIMILARITE LOCALE POUR LE CALCUL DES CARACTERISTIQUES D'UNE COUCHE LIMITE LAMINAIRE DE LIQUIDEPOPKOV AN.1977; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1977; VOL. 20; NO 2; PP. 136-139; BIBL. 3 REF.Article

FREE CONVECTION EFFECTS ON THE UNSTEADY LAMINAR BOUNDARY-LAYER FLOW PAST A POROUS LIMITING SURFACE WITH UNIFORM SUCCION IN STELLAR ATMOSPHERESPANDE GC; GEORGANTOPOULOS GA; GOUDAS CL et al.1979; ASTROPHYS. SPACE SCI.; NLD; DA. 1979; VOL. 60; NO 1; PP. 125-171; BIBL. 34 REF.Article

COUCHE LIMITE LAMINAIRE DANS UN GAZ REELSTYCZEK A.1978; ARCH. BUDOWY MASZ.; POLSKA; DA. 1978; VOL. 25; NO 1; PP. 236-244; ABS. RUSSE ANGL.; BIBL. 4 REF.Article

CARACTERISTIQUES DE LA COUCHE LIMITE LAMINAIRE POUR UNE TURBULENCE ACCRUE DU COURANT EXTERNEDYBAN EP; EHPIK EH YA; SUPRUN TT et al.1976; TEPLOFIZ. I TEPLOTEKH., U.S.S.R.; S.S.S.R.; DA. 1976; NO 30; PP. 86-90; BIBL. 9 REF.Article

AMPLITUDE-DEPENDENT STABILITY OF BOUNDARY-LAYER FLOW WITH A STRONGLY NON-LINEAR CRITICAL LAYERBODONYI RJ; SMITH FT; GAJJAR J et al.1983; IMA JOURNAL OF APPLIED MATHEMATICS; ISSN 0272-4960; GBR; DA. 1983; VOL. 30; NO 1; PP. 1-19; BIBL. 15 REF.Article

STABILITE D'UN ECOULEMENT PLAN PRES DU POINT CRITIQUE DANS LE CAS DE FORTE INSUFFLATIONEROSHENKO VM; ZAJCHIK LI; RABOVSKIJ VB et al.1982; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1982; NO 2; PP. 157-158; BIBL. 8 REF.Article

VORTEX STRUCTURE IN LAMINAR BOUNDARY LAYERS ON A CONCAVE WALLWINOTO SH; CRANE RI.1980; INT. J. HEAT FLUID FLOW; ISSN 0142-727X; GBR; DA. 1980; VOL. 2; NO 4; PP. 221-231; BIBL. 26 REF.Article

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

EQUATIONS DE LA COUCHE LIMITE LAMINAIRE DANS UN MILIEU A DEUX PHASESSTULOV VP.1979; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1979; NO 1; PP. 51-60; BIBL. 10 REF.Article

MODELE SPATIAL D'UNE COUCHE LIMITE LAMINAIRE SUBISSANT UNE CHUTE DE PRESSION DANS LES DIRECTIONS LONGITUDINALE ET TRANSVERSALEPAVLOV VG.1979; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1979; NO 2; PP. 56-62; BIBL. 6 REF.Article

CALCUL D'UNE COUCHE LIMITE LAMINAIRE, D'APRES DES DONNEES EXPERIMENTALES DE REPARTITION DES PRESSIONSOSORGIN VD; POPKOV AN; SIDOROV OP et al.1978; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1978; VOL. 21; NO 4; PP. 88-93; BIBL. 3 REF.Article

METHODE DE LA SIMILITUDE GENERALISEE DANS LA THEORIE DE LA COUCHE LIMITE INSTATIONNAIRE AVEC EQUATION UNIVERSELLE SOUS FORME DIFFERENTIELLEBUSHMARIN ON; STOLETOV VM.1978; INZHENER.-FIZ. ZH., BELORUS. S.S.R.; S.S.S.R.; DA. 1978; VOL. 34; NO 2; PP. 281-287; ABS. ANGL.; BIBL. 5 REF.Article

LAMINAR BOUNDARY-LAYER BEHAVIOUR ON CONTINUOUS, ACCELERATING SURFACES.VLEGGAAR J.1977; CHEM. ENGNG SCI.; G.B.; DA. 1977; VOL. 32; NO 12; PP. 1517-1525; BIBL. 5 REF.Article

SOME SPECIAL BOUNDARY LAYER PROBLEMS.YOUNG AD.1977; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DTSCH.; DA. 1977; VOL. 1; NO 6; PP. 401-414; ABS. ALLEM.; BIBL. 30 REF.Article

INDAGINE SPERIMENTALE SULL' INFLUENZA DI UN VORTICE INDOTTO SULLE PERDITE DI PRESSIONE TOTALE IN UNA SCHIERA DI PALE A BASSA VELOCITA = ETUDE EXPERIMENTALE DE L'INFLUENCE D'UN GENERATEUR DE VORTEX SUR LES PERFORMANCES D'UNE GRILLE D'AUBESSALEMI C.1977; TEC. ITAL.; ITA; DA. 1977; VOL. 42; NO 2; PP. 79-88; ABS. ENG; BIBL. 6 REF.Article

COMPRESSIBLE LAMINAR BOUNDARY LAYERS WITH LARGE ACCELERATION AND COOLING.BACK LH; CUFFEL RF.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 7; PP. 968-971; BIBL. 13 REF.Article

ON THE STABILITY OF THE BOUNDARY LAYER ALONG A CONCAVE WALL.HERBERT T.1976; ARCH. MECH.; POLAND; DA. 1976; VOL. 28; NO 5-6; PP. 1039-1055; ABS. POL. RUSSE; BIBL. 20 REF.Article

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