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

Théorie du décollement de la couche limite laminaire dans un écoulement supersoniqueLIPATOV, I. I.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1984, Num 4, pp 51-56, 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

Effects on Boundary Layer Caused by Inclusion of Dimples at Varying DepthsMILLER, Erik C.Journal of aircraft. 2012, Vol 49, Num 4, pp 969-972, issn 0021-8669, 4 p.Article

Boundary layer separation and vortex creation superflow through small orificesSTONE, M; SRIVASTAVA, A. M.Journal of low temperature physics. 1996, Vol 102, Num 5-6, pp 445-459, issn 0022-2291Article

Boundary layer separation of a two-layer rotating flow on an f planeBREVDO, L; MERKINE, L.Proceedings of the royal society of London, series A : mathematical and physical sciences. 1985, Vol 400, Num 1818, pp 75-95, issn 0080-4630Article

Investigations of turbulent boundary layer in the vicinity of separationKAZIMIERSKI, Z; WYSOCKI, W; SMOLNY, A et al.Archives of Mechanics. 1984, Vol 36, Num 4, pp 523-538, issn 0373-2029Article

Separation criteria for three-dimensional boundary-layer calculationsRAVEN, H. C.AIAA journal. 1984, Vol 22, Num 4, pp 554-556, issn 0001-1452Article

An experimental study of rotating stall in a multistage axial-flow compressorDAS, D. K; JIANG, H. K.Journal of engineering for gas turbines and power. 1984, Vol 106, Num 3, pp 542-551, issn 0742-4795Conference Paper

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

Marginal separation of a three-dimensional boundary layer on a line of symmetryBROWN, S. N.Journal of Fluid Mechanics. 1985, Vol 158, pp 95-111, issn 0022-1120Article

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