Particle motions in sheared suspensions XII. Deformation and burst of fluid drops in shear and hyperbolic flow

1961 ◽  
Vol 16 (3) ◽  
pp. 238-261 ◽  
Author(s):  
F.D Rumscheidt ◽  
S.G Mason
1965 ◽  
Vol 43 (7) ◽  
pp. 1269-1287 ◽  
Author(s):  
C. E. Chaffey ◽  
M. Takano ◽  
S. G. Mason

The angular velocity of a body of revolution suspended in a viscous fluid undergoing slow arbitrary shear flow is given. Integrated equations are derived for the orientation of its axis, directly in terms of the vorticity and dilatation components, for any flow in which the vorticity is parallel to a principal axis of dilatation; these are analogous to the equations for motion of a spheroid in Couette flow with an electric field parallel or perpendicular to the vorticity. The flows considered include examples of hyperbolic–parabolic, elliptic–spiral, and hyperbolic–logarithmic flows in three dimensions, as well as all two-dimensional shear flows.The behavior of certain bodies of revolution that remain stationary in Couette flow is discussed. Translational orbits of asymmetric bodies of revolution in Couette flow are calculated.The behavior of particles in some important shear flows is described, the theory of rotation in hyperbolic flow being developed in detail and confirmed experimentally with rods and disks. Comparison of equivalent ellipsoidal axis ratios obtained from Couette-flow and hyperbolic-flow measurements shows that the former are more accurate if the particle deviates greatly from the spherical shape.


Soft Matter ◽  
2016 ◽  
Vol 12 (36) ◽  
pp. 7688-7697 ◽  
Author(s):  
Tyler Olsen ◽  
Ahmed Helal ◽  
Gareth H. McKinley ◽  
Ken Kamrin

2012 ◽  
Vol 693 ◽  
pp. 345-366 ◽  
Author(s):  
L. Jibuti ◽  
S. Rafaï ◽  
P. Peyla

AbstractIn this paper, we conduct a numerical investigation of sheared suspensions of non-colloidal spherical particles on which a torque is applied. Particles are mono-dispersed and neutrally buoyant. Since the torque modifies particle rotation, we show that it can indeed strongly change the effective viscosity of semi-dilute or even more concentrated suspensions. We perform our calculations up to a volume fraction of 28 %. And we compare our results to data obtained at 40 % by Yeo and Maxey (Phys. Rev. E, vol. 81, 2010, p. 62501) with a totally different numerical method. Depending on the torque orientation, one can increase (decrease) the rotation of the particles. This results in a strong enhancement (reduction) of the effective shear viscosity of the suspension. We construct a dimensionless number $\Theta $ which represents the average relative angular velocity of the particles divided by the vorticity of the fluid generated by the shear flow. We show that the contribution of the particles to the effective viscosity can be suppressed for a given and unique value of $\Theta $ independently of the volume fraction. In addition, we obtain a universal behaviour (i.e. independent of the volume fraction) when we plot the relative effective viscosity divided by the relative effective viscosity without torque as a function of $\Theta $. Finally, we show that a modified Faxén law can be equivalently established for large concentrations.


2007 ◽  
Vol 19 (12) ◽  
pp. 128106
Author(s):  
C. A. Langer ◽  
E. Akylas ◽  
S. C. Kassinos

AIChE Journal ◽  
1997 ◽  
Vol 43 (6) ◽  
pp. 1436-1447 ◽  
Author(s):  
J. J. M. Janssen ◽  
A. Boon ◽  
W. G. M. Agterof

1968 ◽  
Vol 19 (2) ◽  
pp. 105-126 ◽  
Author(s):  
D. F. Myring ◽  
A. D. Young

SummaryFor boundary layer flows over curved surfaces at moderately high supersonic speeds the existence of normal pressure gradients within the boundary layer becomes important even for small curvatures and they cannot be ignored. The describing equations are basically parabolic in form so that the simplifications inherent in hyperbolic flows would not at first sight seem to be relevant. However, the equations of motion for a two-dimensional, supersonic, rotational, viscous flow are analysed along the lines of a hyperbolic flow and the individual effects of viscosity and vorticity are examined with regard to the isobar distributions. It is found that these two properties have compensating effects and the experimental evidence presented confirms the conclusion that inside the boundary layer the isobars follow much the same rules as those which determine the isobars in the external hyperbolic flow. Since for turbulent boundary layers the fullness of the Mach number profile produces almost linear Mach lines in the boundary layer, this provides a simple extension to the methods of analysis, and the momentum integral equation is reformulated using a swept element bounded by linear isobars. The final equation is similar in form to the conventional one except that the momentum and displacement thicknesses are now defined by integrals along the swept isobars, and all normal pressure gradients due to centrifugal effects are accounted for.


2014 ◽  
Vol 58 (1) ◽  
pp. 237-254 ◽  
Author(s):  
Sylvie Van Loon ◽  
Jan Fransaer ◽  
Christian Clasen ◽  
Jan Vermant

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