INFLUENCE DU DEGRE DE TURBULENCE DE L'ECOULEMENT INCIDENT SUR LA COUCHE LIMITE TRIDIMENSIONNELLEBURLAKA VV; GRECHANICHENKO YU V.1983; TEPLOENERGETIKA (MOSKVA, 1954); ISSN 0040-3636; SUN; DA. 1983; NO 7; PP. 62-64; BIBL. 5 REF.Article

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A METHOD FOR THE CALCULATION OF 3D BOUNDARY LAYERS ON PRACTICAL WING CONFIGURATIONSLINDHOUT JPF; MOEK G; DE BOER E et al.1981; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1981; VOL. 103; NO 1; PP. 104-111; BIBL. 14 REF.Article

THREE-DIMENSIONAL LAMINAR BOUNDARY LAYERS AND THE OK OF ACCESSIBILITYCEBECI T; KHATTAB AK; STEWARTSON K et al.1981; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1981; VOL. 107; PP. 57-87; BIBL. 2 P.Article

SUR UNE COUCHE LIMITE TRIDIMENSIONNELLE NON STATIONNAIRE EN INTERACTION LIBRE AVEC UN ECOULEMENT EXTERNERYZHOV OS.1980; PRIKL. MAT. MEH.; ISSN 0032-8235; SUN; DA. 1980; VOL. 44; NO 6; PP. 1035-1052; BIBL. 14 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

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

CORRELATION OF THE DETACHMENT OF TWO-DIMENSIONAL TURBULENT BOUNDARY LAYERSKLINE SJ; BARDINA JG; STRAWN RC et al.1983; AIAA J.; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 1; PP. 68-73; BIBL. 31 REF.Article

THREE-DIMENSIONAL WING BOUNDARY LAYER CALCULATED WITH EIGHT DIFFERENT METHODSHUMPHREYS DA.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 2; PP. 232-234; BIBL. 15 REF.Article

WALL REGION OF A RELAXING THREE-DIMENSIONAL INCOMPRESSIBLE TURBULENT BOUNDARY LAYER.HEBBAR KS; MELNIK WL.1978; J. FLUID MECH.; G.B.; DA. 1978; VOL. 85; NO 1; PP. 33-56; BIBL. 1 P.Article

PROGRES DANS LES METHODES DE CALCUL DES COUCHES LIMITES TURBULENTES BI ET TRIDIMENSIONNELLES.COUSTEIX J.1976; OFF. NATION. ET. RECH. AEROSPAT., NOTE TECH.; FR.; DA. 1976; NO 15; PP. 1-28; ABS. ANGL.; BIBL. 2 P.Serial Issue

ETUDE EXPERIMENTALE DE LA COUCHE LIMITE TRIDIMENSIONNELLE SUR LE FOND DU CANAL DES GRILLES DE TURBINEGRECHANICHENKO YU V; NESTERENKO VA; BURLAKA VV et al.1982; TEPLOENERGETIKA (MOSKVA, 1954); ISSN 0040-3636; SUN; DA. 1982; NO 9; PP. 53-55; BIBL. 6 REF.Article

AGREEMENT OF HIGH CONICAL FLOW THEORY WITH EXPERIMENTAL RESULTS FOR SUPERSONIC FLOWNASTASE A.1980; Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1980; VOL. 60; NO 7; PP. T199-T201; BIBL. 8 REF.Article

MEASURED REYNOLDS STRESS TENSORS IN A THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER.EZEKWE CI; PIERCE FJ; MCALLISTER JE et al.1978; A.I.A.A. J., NEW YORK; USA; DA. 1978; VOL. 16; NO 7; PP. 645-646; BIBL. 10 REF.Article

QUELQUES EFFETS APPARAISSANT LORS DU CONTROLE DE LA COUCHE LIMITE SUR UNE ZONE DE LA SURFACEGUREVICH YU G; SHAL'MAN E YU.1978; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1978; NO 4; PP. 3-9; BIBL. 6 REF.Article

WALL SHEAR STRESS PREDICTION IN THREE-DIMENSIONAL TURBULENT BOUNDARY LAYERSSWAMY NVC; ASWATHA NARAYANA PA.1977; APPL. SCI. RES.; NLD; DA. 1977; VOL. 33; NO 5-6; PP. 471-480; BIBL. 15 REF.Article

CHARACTERISTICS OF MEAN VELOCITY IN THE ANNULUS WALL REGION AT THE EXIT OF TURBOMACHINERY ROTOR PASSAGEDAVINO R; LAKSHMINARAYANA B.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 10 P.; BIBL. 10 REF.Conference Paper

SOLUTION-ADAPTIVE GRID FOR THE CALCULATION OF THREE-DIMENSIONAL LAMINAR AND TURBULENT BOUNDARY LAYERSMELNIK WL.1982; LECT. NOTES PHYS.; ISSN 0075-8450; DEU; DA. 1982; VOL. 170; PP. 377-382; BIBL. 9 REF.Conference Paper

SOME ASPECTS OF THREE-DIMENSIONAL LAMINAR BOUNDARY LAYERSDWYER HA.1981; ANNU. REV. FLUID MECH.; ISSN 0066-4189; USA; DA. 1981; VOL. 13; PP. 217-229; BIBL. 21 REF.Article

A PREDICTION METHOD FOR TURBULENT BOUNDARY LAYERS ON SHIP HULLS AT ZERO FRONDE NUMBER = METHODE DE PREVISION DES COUCHES LIMITES TURBULENTES SUR DES COQUES DE NAVIRE A UN NOMBRE DE FRONDE NULKROGSTAD PA.1981; NORW. MARIT. RES.; ISSN 0304-1743; NOR; DA. 1981; VOL. 9; NO 1; PP. 21-33; BIBL. 22 REF.Article

PREDICTIONS OF TWO-DIMENSIONAL BOUNDARY LAYERS WITH THE AID OF THE K-EPSILON MODEL OF TURBULENCESINGHAL AK; SPALDING DB.1981; COMPUT. METHODS APPL. MECH. ENG.; ISSN 0045-7825; NLD; DA. 1981; VOL. 25; NO 3; PP. 365-383; BIBL. 29 REF.Article

ANALYSE ASYMPYTOTIQUE DES EQUATIONS D'UNE COUCHE LIMITE A TROIS DIMENSIONSSHAL'MAN E YU.1979; IZV. AKAD. NAUK S.S.S.R., MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1979; NO 5; PP. 155-157; BIBL. 6 REF.Article

THE THREE-DIMENSIONAL BOUNDARY LAYER ON A ROTATING FLAT PLATE AS INFLUENCED BY THE CONTAINING END-WALLSEKEROL H; RAILLY JW.1981; INT. J. HEAT FLUID FLOW; ISSN 0142-727X; GBR; DA. 1981; VOL. 2; NO 1; PP. 35-40; BIBL. 5 REF.Article