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140<br />
Stability of dusty gas flow in a vertical channel<br />
S.A. Boronin a, A.N. Osiptsov a<br />
The problem of laminar-turbulent transition in 2D dusty-gas flows was<br />
considered in a number of studies using the Saffman 1 formulation or its small<br />
modifications 2 , in which velocity slip of the phases in the basic flow was<br />
ignored. It was shown that the presence of even a small amount of particles<br />
can significantly change the limits of the laminar flow regime. In the present<br />
study, dealing with the stability of a vertical channel flow with inertial particles,<br />
we modify the Saffman formulation and focus on the role of phase velocity<br />
slip in the basic flow (caused by the gravity force) in laminar-turbulent<br />
transition.<br />
We consider the linear stability of downward dusty-gas flow in a vertical<br />
channel within the two-fluid model 3 with Stokes particles. The basic carrierphase<br />
flow is given by the Poiseuille velocity profile, with the particle velocity<br />
slip being equal to the gravitational settling velocity. The disturbances are<br />
specified in the form of travelling waves. After the linearization, the problem is<br />
reduced to a modified Orr-Sommerfeld equation with several extra terms. The<br />
eigenvalues are calculated numerically at high accuracy using an<br />
orthonormalization method.<br />
The effect of the particles on the gas flow is described by three similarity<br />
parameters: Froude number (which determines the velocity slip in the basic<br />
flow), particle mass loading , and inverse Stokes number (ratio of the<br />
channel width to the particle velocity relaxation length). A parametric study of<br />
neutral curves was performed for fixed =0.1. It was shown that: (i) for <<br />
0.075 (high-inertia particles), the critical Reynolds number decreases as<br />
compared to horizontal channel flow and the effect of particles is most<br />
pronounced at small Froude numbers (high gravity). (ii) For 0.075, the<br />
instability region in the (Re, k) plane (Re – basic-flow Reynolds number, k –<br />
wave number) becomes bounded and reduces (tending to a point) as the<br />
Froude number decreases and tends to a threshold value Fr 0.. Accordingly, for<br />
Fr < Fr 0 the flow is stable with respect to arbitrary small perturbations. The<br />
work was supported by the RFBR (project 05-01-00502).<br />
a<br />
Institute of <strong>Mechanics</strong> Lomonosov Moscow State University, Michurinskii pr., 1 119899 Moscow,<br />
Russia<br />
1 Saffman, J. Fluid Mech. 13, 120 (1962).<br />
2 Asmolov and Manuilovich, J. Fluid Mech. 365, 135 (1998)<br />
3 Marble, Ann. Rev. Fluid Mech. 2, 397 (1970)