Calcul de la chute critique de pression sur un échelon de densité produit lors du décollement d'une couche limite turbulenteTAGIROV, R. K.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1985, Num 4, pp 38-45, issn 0568-5281Article

A new multifold series general solution of the steady, laminar boundary layers (3rd report, extension of the solution to the case of not smoothly joining mainstream-velocities)ISHIZAWA, S.Bulletin of the JSME. 1983, Vol 26, Num 222, pp 2081-2090, issn 0021-3764Article

The detachment region location using the turbulent fluctuation intensity criterionDUMITRESCU, H; SAVULESCU, S. N.Revue roumaine des sciences techniques. Série de mécanique appliquée. 1984, Vol 29, Num 6, pp 569-576, issn 0035-4074Article

Caractéristiques géométriques du décollement de la couche limite turbulente lors de l'interaction avec une discontinuité linéaire de condensation dans les écoulements coniquesZUBIN, M. A; OSTAPENKO, N. A.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1983, Num 6, pp 43-51, issn 0568-5281Article

Numerical computation of unsteady laminar boundary layers with separation using two-parameter integral methodMATSUSHITA, M; MURATA, S; AKAMATSU, T et al.Bulletin of the JSME. 1985, Vol 28, Num 245, pp 2630-2638, issn 0021-3764Article

DREIKOMPONENTENMESSUNGEN AM MODELL EINES LEICHTEN STOL-FLUGZEUGS MIT AUSBLASEN IN FLUEGELTIEFENRICHTUNG. = MESURES A TROIS COMPOSANTES SUR UNE MAQUETTE D'AVION LEGER DE TYPE ADAC AVEC SOUFFLAGE A L'INTERIEUR DE L'AILEKORNER H; LOHR R.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 74; PP. 1-21; ABS. ANGL.; BIBL. 8 REF.Serial Issue

Etude numérique du décollement bidimensionnel basée sur les équations de Navier-StokesMARTSINKOVSKI, V; SHKADOV, V. YA.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1985, Num 1, pp 26-32, issn 0568-5281Article

Unsteady flow concepts for dynamic stall analysisERICSSON, L. E; REDING, J. P.Journal of aircraft. 1984, Vol 21, Num 8, pp 601-606, issn 0021-8669Article

Two-dimensional separating turbulent boundary layersSCHOFIELD, W. H.AIAA journal. 1986, Vol 24, Num 10, pp 1611-1620, issn 0001-1452Article

Concerning upstream influence in separating boundary layers on downstream influence in channel flowSMITH, F. T.Quarterly Journal of Mechanics and Applied Mathematics. 1984, Vol 37, Num 3, pp 389-399, issn 0033-5614Article

Numerical computation of unsteady laminar boundary layers with separation using one-parameter integral method. II: The separation singularity in unsteady boundary layerMATSUSHITA, M; AKAMATSU, T.Bulletin of the JSME. 1985, Vol 28, Num 240, pp 1044-1049, issn 0021-3764Article

Bulk flow parameters in turbulent wall boundary layers near separationYAHYA SALAM, M.Applied scientific research. 1986, Vol 43, Num 1, pp 23-38, issn 0003-6994Article

The prediction of separated flow using a viscous-inviscid interaction methodWILLIAMS, B. R.Aeronautical Journal. 1985, Vol 89, Num 885, pp 185-197, issn 0001-9240Article

A mathematically simple turbulence closure model for attached and separated turbulent boundary layersJOHNSON, D. A; KING, L. S.AIAA journal. 1985, Vol 23, Num 11, pp 1684-1692, issn 0001-1452Article

Applicability of the independence principle to subsonic turbulent flow over a swept rearward-facing stepSELBY, G. V.AIAA journal. 1983, Vol 21, Num 11, pp 1603-1604, issn 0001-1452Article

Boundary layer separation singularities for an upstream moving wallVAN DOMMELEN, L. L; SHEN, S. F.Acta mechanica. 1983, Vol 49, Num 3-4, pp 241-254, issn 0001-5970Article

INTERACTION D'UNE COUCHE LIMITE TURBULENTE AVEC UN SAUT DE DENSITE A DES VITESSES TRANSONIQUES DE L'ECOULEMENTVELICHKO SA; LIFSHISHCH YU B.1983; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1983; NO 2; PP. 32-38; BIBL. 17 REF.Article

EFFET D'AMPLIFICATION DE LA PUISSANCE DANS UN COMPOSANT FLUIDIQUE A ECOULEMENT DIRECT A PARTIR DU PRINCIPE DU DECOLLEMENT DE LA COUCHE LIMITELEBEDEV VP; MYAGKOV VI; KOPKOV GA et al.1973; IZVEST. VYSSH. UCHEBN. ZAVED., MASH.-STR.; S.S.S.R.; DA. 1973; NO 12; PP. 73-76; BIBL. 4 REF.Article

NEAR-WAKES OF ELLIPTIC CYLINDERS IN SUBCRITICAL FLOW.MODI VJ; DIKSHIT AK.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 490-497; BIBL. 28 REF.Article

BOUNDARY-LAYER SEPARATION IN UNSTEADY FLOW.SEARS WR; TELIONIS DP.1975; S.I.A.M. J. APPL. MATH.; U.S.A.; DA. 1975; VOL. 28; NO 1; PP. 215-235; BIBL. 1 P. 1/2Article

NEW DIAGNOSTIC TECHNIQUE FOR THE STUDY OF TURBULENT BOUNDARY-LAYER SEPARATION.HORSTMAN CC; OWEN FK.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1437-1438; BIBL. 4 REF.Article

TURBULENT BOUNDARY-LAYER FLOW SEPARATION MEASUREMENTS USING HOLOGRAPHIC INTERFEROMETRY.HAVER AG; RADLEY RJ JR.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1071-1075; BIBL. 5 REF.Article

EVALUATION OF SEVERAL APPROXIMATE MODELS FOR LAMINAR INCOMPRESSIBLE SEPARATION BY COMPARISON WITH COMPLETE NAVIER-STOKES SOLUTION. = EVALUATION DE PLUSIEURS MODELES APPROCHES DE DECOLLEMENT INCOMPRESSIBLE LAMINAIRE PAR COMPARAISON AVEC LA SOLUTION DE NAVIER-STOKES COMPLETEGHIA KN; GHIA U; TESCH WA et al.1975; A.G.A.R.D. CONF. PROC.; FR.; DA. 1975; NO 168; PP. 6.1-6.15; BIBL. 14 REF.; (FLOW SEP. FLUID DYN. PANEL SYMP.; GOETTINGEN, GER.; 1975)Conference Paper

HEMISPHERE-CYLINDER IN TRANSONIC FLOW, MINFINI=0.7 EQUIV. A 1.0.TSUING HSIEH.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1411-1413; BIBL. 3 REF.Article

Page / 23