Local transition to turbulence behind an obstacle for a nominally laminar flow

2016 ◽  
Vol 37 (3) ◽  
pp. 360-367 ◽  
Author(s):  
A. B. Mazo ◽  
D. I. Okhotnikov
2012 ◽  
Vol 134 (2) ◽  
Author(s):  
N. Vinod ◽  
Rama Govindarajan

The secondary instability of the incompressible boundary layer in the axial flow past a cylinder is studied. The laminar flow is shown to be always stable at high transverse curvatures to secondary disturbances. Because the primary mode is stable as well, (Tutty et al., 2002, “Boundary Layer Flow on a Long Thin Cylinder,”. Phys. Fluids, 14(2), pp. 628–637), this implies that the boundary layer on a thin long cylinder may undergo transition to turbulence by means very different from that on a flat plate. The azimuthal wavenumber of the least stable secondary modes (m±) are related to that of the primary (n) by m+ = 2n and m− = −n. The base flow is shown to be inviscidly stable at any curvature.


2017 ◽  
Vol 818 ◽  
pp. 595-622
Author(s):  
Emmanuel Plaut ◽  
Nicolas Roland ◽  
Chérif Nouar

In order to model the transition to turbulence in pipe flow of non-Newtonian fluids, the influence of a strongly shear-thinning rheology on the travelling waves with a threefold rotational symmetry of Faisst & Eckhardt (Phys. Rev. Lett., vol. 91, 2003, 224502) and Wedin & Kerswell (J. Fluid Mech., vol. 508, 2004, pp. 333–371) is analysed. The rheological model is Carreau’s law. Besides the shear-thinning index $n_{C}$, the dimensionless characteristic time $\unicode[STIX]{x1D706}$ of the fluid is considered as the main non-Newtonian control parameter. If $\unicode[STIX]{x1D706}=0$, the fluid is Newtonian. In the relevant limit $\unicode[STIX]{x1D706}\rightarrow +\infty$, the fluid approaches a power-law behaviour. The laminar base flows are first characterized. To compute the nonlinear waves, a Petrov–Galerkin code is used, with continuation methods, starting from the Newtonian case. The axial wavenumber is optimized and the critical waves appearing at minimal values of the Reynolds number $\mathit{Re}_{w}$ based on the mean velocity and wall viscosity are characterized. As $\unicode[STIX]{x1D706}$ increases, these correspond to a constant value of the Reynolds number based on the mean velocity and viscosity. This viscosity, close to the one of the laminar flow, can be estimated analytically. Therefore the experimentally relevant critical Reynolds number $\mathit{Re}_{wc}$ can also be estimated analytically. This Reynolds number may be viewed as a lower estimate of the Reynolds number for the transition to developed turbulence. This demonstrates a quantified stabilizing effect of the shear-thinning rheology. Finally, the increase of the pressure gradient in waves, as compared to the one in the laminar flow with the same mass flux, is calculated, and a kind of ‘drag reduction effect’ is found.


1970 ◽  
Vol 92 (4) ◽  
pp. 732-739 ◽  
Author(s):  
R. J. Goldstein ◽  
V. L. Eriksen ◽  
R. M. Olson ◽  
E. R. G. Eckert

Results of an experimental investigation of the laminar flow of air over a downstream-facing step are presented. The experiments include visual observations of smoke filaments (in the viscous layer), qualitative velocity fluctuation measurements, and mean velocity profiles. Results are reported over a range of 0.36 – 1.02 cm in step height, 0.61 – 2.44 m/sec in free stream velocity at the step, and 0.16 – 0.51 cm in boundary layer displacement thickness at the step. Laminar flow to reattachment of a free shear layer is observed for subsonic flow and two criteria for which transition to turbulence at reattachment exists are presented. The laminar reattachment length is not a constant number of step heights as for turbulent flow, but varies with Reynolds number and boundary layer thickness at the step. The shape of the velocity profile at reattachment is found to be similar to the shape of a laminar boundary layer profile at separation and the boundary layer profiles downstream of reattachment are similar to those in a laminar boundary layer developing toward separation except that they are traversed in the reverse sense.


1990 ◽  
Vol 64 (10) ◽  
pp. 1111-1114 ◽  
Author(s):  
Shoichi Kai ◽  
Walter Zimmermann ◽  
Masanori Andoh ◽  
Nobuyuki Chizumi

2009 ◽  
Vol 627 ◽  
pp. 215-233 ◽  
Author(s):  
D. VISWANATH ◽  
P. CVITANOVIĆ

Lower branch travelling waves and equilibria computed in pipe flow and other shear flows appear intermediate between turbulent and laminar motions. We take a step towards connecting these lower branch solutions to transition by deriving a numerical method for finding certain special disturbances of the laminar flow in a short pipe. These special disturbances cause the disturbed velocity field to approach the lower branch solution by evolving along its stable manifold. If the disturbance were slightly smaller, the flow would relaminarize, and if slightly larger, it would transition to a turbulent state.


1977 ◽  
Vol 99 (4) ◽  
pp. 693-698 ◽  
Author(s):  
N. A. Feliss ◽  
M. C. Potter ◽  
M. C. Smith

This paper complements an earlier paper by Karnitz, Potter, and Smith [1] (1974) in which the mechanism of the transition of a plane Poiseuille flow between parallel plates was examined. In the present investigation an experimental critical Reynolds number of 7500 (based on average velocity and channel height) was achieved at which the flow became unstable and transition to turbulence occurred. The linear theoretical Reynolds number of 7700 for instability appears to be a simple extrapolation of the present data as the disturbance intensity is allowed to shrink to zero. Bursting (an alternating turbulent to laminar flow) was observed at transition. The transient changes in the velocity profile when the flow is intermittent between a turbulent burst and a laminar flow were observed. The major portion of the burst profile is characteristic of the one-seventh power law profile common to fully turbulent flow. Disturbances were observed to amplify to turbulent bursts in the wall boundary layers in the entrance region of the channel in high Reynolds number flows (the Reynolds number must exceed the critical Reynolds number by a sufficient amount). Thus, the wall boundary layer becomes unstable, resulting in a transition to turbulence before the flow becomes fully developed at sufficiently high Reynolds numbers.


Sign in / Sign up

Export Citation Format

Share Document