kw.\*:("LAMINAR WAKE")
Results 1 to 19 of 19
Selection :
TRANSITION TO TURBULENCE IN TWO-DIMENSIONAL WAKESDEMETRIADES A.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 6; PP. 587-591; BIBL. 19 REF.Article
AXISYMMETRIC LAMINAR WAKE BEHIND A SLENDER BODY OF REVOLUTION.HAMA FR; PETERSON LE.1976; J. FLUID MECH.; G.B.; DA. 1976; VOL. 76; NO 1; PP. 1-15; BIBL. 14 REF.Article
BULBES DE RECIRCULATION AU SEIN D'UN SILLAGE.WERLE H; SOLIGNAC JL.1977; RECH. AEROSPAT.; FR.; DA. 1977; NO 1; PP. 15-30; ABS. ANGL.; BIBL. 7 REF.Article
Développement d'un sillage à impulsion excédentaire nulleKOROBKO, V. I; SHASHMIN, V. K; SHUL'MAN, Z. P et al.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1984, Num 3, pp 27-33, issn 0568-5281Article
EXPERIMENTS ON THE ROLE OF AMPLITUDE AND PHASE MODULATIONS DURING TRANSITION TO TURBULENCEMIKSAD RW; JONES FL; POWERS EJ et al.1982; J. FLUID MECH.; ISSN 0022-1120; GBR; DA. 1982-10; VOL. 123; PP. 1-29; BIBL. 16 REF.Article
EFFET DE LA VISCOSITE SUR LES VAGUES. RESISTANCE DU NAVIRE DANS UN FLUIDE VISQUEUX A SURFACE LIBRE. IIKINOSHITA T; MARVO H; NITOH M et al.1979; J. SOC. NAV. ARCHIT. JPN.; ISSN 0514-8499; JPN; DA. 1979; VOL. 146; PP. 9-17; ABS. ENG; BIBL. 11 REF.Article
A THEORETICAL INVESTIGATION OF LAMINAR WAKES BEHIND AIRFOILS AND THE RESULTING NOISE PATTERN.FATHY A; RASHED MI; LUMSDAINE E et al.1977; J. SOUND VIBR.; G.B.; DA. 1977; VOL. 50; NO 1; PP. 133-144; BIBL. 10 REF.Article
CONVECTIVE HEAT- AND MASS-TRANSFER IN HYPERSONIC NEAR WAKESSKURIN LI; YURKIN AV.1978; HEAT TRANSFER, SOVIET RES.; USA; DA. 1978; VOL. 10; NO 5; PP. 95-101; BIBL. 2 REF.Article
DEVELOPMENT OF CONFINED LAMINAR WAKES AT LARGE REYNOLDS NUMBERPLOTKIN A.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 8 P.; BIBL. 11 REF.Conference Paper
An experimental investigation of the flow around a circular cylinder : influence of aspect ratioNORBERG, C.Journal of Fluid Mechanics. 1994, Vol 258, pp 287-316, issn 0022-1120Article
Visualization of the spanwise cellular structure of the laminar wake of wall-bounded circular cylindersKÖNIG, M; EISENHOHR, H; ECKELMANN, H et al.Physics of fluids. A, Fluid dynamics. 1992, Vol 4, Num 5, pp 869-872, issn 0899-8213Article
Development of instability in the wake of a plate positioned parallel to the flowKUIBIN, P. A; RUDYAK, V. YA.Fluid dynamics. 1992, Vol 27, Num 1, pp 19-23, issn 0015-4628Article
Numerical Study of Two-Dimensional Circular Cylinders in Tandem at Moderate Reynolds NumbersVAKIL, Ali; GREEN, Sheldon I.Journal of fluids engineering. 2013, Vol 135, Num 7, issn 0098-2202, 071204.1-071204.9Article
Different modes of vortex shedding : An overviewZDRAVKOVICH, M. M.Journal of fluids and structures. 1996, Vol 10, Num 5, pp 427-437, issn 0889-9746Article
An extension of Roe's Riemann solver applied to reactive viscous flows for the computation of laminar hypersonic wake = Une extension du solveur de Riemann approche de Roe appliqué au calcul d'un écoulement visqueux réactif pour un sillage laminaire hypersonicDubroca, Bruno.1993, 13 p.Report
Discrete shedding modes in the von Kármán vortex streetKÖNIG, M; NOACK, B. R; ECKELMANN, H et al.Physics of fluids. A, Fluid dynamics. 1993, Vol 5, Num 7, pp 1846-1848, issn 0899-8213Article
Experimentelle Untersuchung des dreidimensionalen Nachlaufs zylindrischer Körper bei kleinen Reynoldszahlen = Experimental investigation of the 3D-wake of circular cylinders at low Reynolds numbersKÖNIG, M.Mitteilungen aus dem Max-planck Institut für Stromungsforschung und der Aerodynamischen Versuchsanstalt. 1993, Num 111, pp I-III, issn 0374-1257Article
The stability of two-dimensional wakes and shear layers at high mach numbersPAPAGEORGIOU, D. T.Physics of fluids. A, Fluid dynamics. 1991, Vol 3, Num 5, pp 793-802, issn 0899-8213, 10 p., p.1Article
The fine structure in the Strouhal-Reynolds number relationship of the laminar wake of a circular cylinderKOÊNIG, M; EISENLOHR, H; ECKELMANN, H et al.Physics of fluids. A, Fluid dynamics. 1990, Vol 2, Num 9, pp 1607-1614, issn 0899-8213, 8 p.Article