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Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

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particle size was studied. In a density-matched suspension, the inertia of the particle <strong>and</strong> that of the fluid are indistinguishable;<br />

hence, the results for the scaling of the stresses may not be applicable to situations in which the densities differ. Additional questions<br />

surround the normal stress, which was measured by using a flexible membrane for the inner stationary cylinder that would<br />

deflect in response to the applied pressure. The system was insensitive to small pressure changes, <strong>and</strong> the membrane deflection<br />

may have altered the gap size <strong>and</strong> the mean solid concentration. The current work at Caltech focuses on experiments <strong>and</strong> simulations<br />

for conditions similar to those originally examined by Bagnold. The low-gravity environment offers the opportunity to reexamine<br />

Bagnold’s experiments for particles of varying densities. These experiments should provide an opportunity to separate the<br />

effects of the inertia of both the fluid <strong>and</strong> solid phases on the shear <strong>and</strong> normal stresses. We plan to conduct experiments using<br />

different particle sizes <strong>and</strong> density, varying particle concentrations <strong>and</strong> shear rates that would extend the Bagnold number well<br />

into the grain inertia regime. In addition, the work involves a computational component that uses a combination of smooth-particle<br />

hydrodynamics <strong>and</strong> the discrete element method to compute liquid-solid flows. The experimental apparatus will consist of a coaxial<br />

shear cell with a rotating outer cylinder. The inner cylinder will be mounted on a friction-free air bearing <strong>and</strong> constrained from<br />

rotation by a load cell to measure the shear force. For the flight instrument, pressure sensors will be inserted in the wall of the inner<br />

cylinder to simultaneously measure the normal force. The granular material <strong>and</strong> the fluid will be contained in the annular region<br />

of the experiment. We have a prototype shear cell already constructed that we are using as a basis for the design of the flight instrument.<br />

In addition to the experimental measurements, the project also involves a computational phase that uses a combination of<br />

the smoothed particle hydrodynamics technique (SPH) <strong>and</strong> the discrete element method (DEM) to model flows containing a viscous<br />

fluid <strong>and</strong> solid macroscopic particles. The two-dimensional numerical simulations are validated by comparing with experimental<br />

measurements for wake size, drag coefficient <strong>and</strong> heat transfer for flow past a circular cylinder at Reynolds numbers up<br />

to approximately 100. The comparisons demonstrate that the technique can be successfully used for incompressible flows at<br />

Reynolds numbers up to approximately 100. The central focus of the work, however, is in computing flows of liquid-solid mixtures.<br />

Hence, the simulations were run for neutrally buoyant particles contained between two shearing plates for different solid<br />

fractions, fluid viscosities <strong>and</strong> shear rates. The simulations involved up to 18 solid particles sheared between two plates separated<br />

by a distance of approximately 8 particle diameters. The no-slip boundary condition was satisfied on the surface of the particles<br />

<strong>and</strong> the bounding walls. The tangential force resulting from the presence of particles shows an increasing dependence on the shear<br />

rate, from a linear regime for macro-viscous flows to a square dependence for grain inertia flows. The normal force showed considerable<br />

variation with time, which is not fully understood <strong>and</strong> is part ongoing numerical simulations. In addition, the simulations<br />

indicated stability problems at higher shear rates; the instability has also been observed in other SPH simulations. Hence, the focus<br />

of the current work involves the effect of the smoothing function <strong>and</strong> other features of the simulation technique on the flow parameters.<br />

Author (revised)<br />

Granular Materials; Hydrodynamics; Interstitials; Viscosity<br />

<strong>2001</strong>0024978 Rennes Univ., France<br />

Sheet Flows, Avalanches, <strong>and</strong> Dune Migration on Earth <strong>and</strong> Mars<br />

Jenkins, J., Cornell Univ., USA; Bideau, D., Rennes Univ., France; Hanes, D., Florida Univ., USA; Proceedings of the Fifth Microgravity<br />

Fluid Physics <strong>and</strong> Transport Phenomena Conference; December 2000, pp. 1355-1364; In English; See also <strong>2001</strong>0024890;<br />

No Copyright; Avail: CASI; A02, Hardcopy; A10, Microfiche<br />

We have begun a study of sheet flows <strong>and</strong> avalanches of granular materials in terrestrial <strong>and</strong> Martian environments. Sheet<br />

flows are relatively thin, highly concentrated regions of grains flowing near the ground under the influence of a strong turbulent<br />

wind. In them, grains are suspended by inter-particle friction, inter-particle collisions, <strong>and</strong>/or the velocity fluctuations of the turbulent<br />

gas. Avalanches are flows of dry, cohesionless granular materials that are driven by gravity down inclines against the frictional<br />

<strong>and</strong> collisional resistance of the grains. The study will employ <strong>and</strong> extend existing theories involving particle-particle <strong>and</strong> gas-particle<br />

interactions to apply to the evolution of a typical terrestrial s<strong>and</strong> dune during a s<strong>and</strong>storm. Experiments will explore the generation<br />

of airborne particles in collisions, the flow of air <strong>and</strong> particles over particle beds, <strong>and</strong> the dependence of the angle of repose<br />

on particle packing <strong>and</strong> friction. We will also investigate the influence of particle size, reduced gravity, gas density, <strong>and</strong> gas viscosity<br />

in order to extend our results to the Martian environment. The focus will be on modeling mechanisms for the transport of granular<br />

materials by the wind <strong>and</strong> gravity. The anticipated result of this activity will be continuum equations for the balance of mass,<br />

momentum, <strong>and</strong> energy for both the particle phase <strong>and</strong> the gas phase that may be employed in numerical codes to study unsteady,<br />

inhomogeneous flows. In the study of suspension <strong>and</strong> transport by the wind, an effort will be made to underst<strong>and</strong> the transition<br />

between successive regimes of flow that are observed as the strength of the wind increases. In particular, the means by which<br />

momentum <strong>and</strong> energy are exchanged between particles <strong>and</strong> between particles <strong>and</strong> the gas will be described <strong>and</strong> quantified. Also,<br />

the interface between the bed <strong>and</strong> the flow will be studied in experiments <strong>and</strong> computer simulations in order to underst<strong>and</strong> better<br />

the balance of momentum <strong>and</strong> energy there. This will lead to improved boundary conditions for the continuum equations. In the<br />

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