25 research outputs found

    A note on Stokes' problem in dense granular media using the μ(I)\mu(I)--rheology

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    The classical Stokes' problem describing the fluid motion due to a steadily moving infinite wall is revisited in the context of dense granular flows of mono-dispersed beads using the recently proposed μ(I)\mu(I)--rheology. In Newtonian fluids, molecular diffusion brings about a self-similar velocity profile and the boundary layer in which the fluid motion takes place increases indefinitely with time tt as νt\sqrt{\nu t}, where ν\nu is the kinematic viscosity. For a dense granular visco-plastic liquid, it is shown that the local shear stress, when properly rescaled, exhibits self-similar behaviour at short-time scales and it then rapidly evolves towards a steady-state solution. The resulting shear layer increases in thickness as νgt\sqrt{\nu_g t} analogous to a Newtonian fluid where νg\nu_g is an equivalent granular kinematic viscosity depending not only on the intrinsic properties of the granular media such as grain diameter dd, density ρ\rho and friction coefficients but also on the applied pressure pwp_w at the moving wall and the solid fraction ϕ\phi (constant). In addition, the μ(I)\mu(I)--rheology indicates that this growth continues until reaching the steady-state boundary layer thickness δs=βw(pw/ϕρg)\delta_s = \beta_w (p_w/\phi \rho g ), independent of the grain size, at about a finite time proportional to βw2(pw/ρgd)3/2d/g\beta_w^2 (p_w/\rho g d)^{3/2} \sqrt{d/g}, where gg is the acceleration due to gravity and βw=(τwτs)/τs\beta_w = (\tau_w - \tau_s)/\tau_s is the relative surplus of the steady-state wall shear-stress τw\tau_w over the critical wall shear stress τs\tau_s (yield stress) that is needed to bring the granular media into motion... (see article for a complete abstract).Comment: in press (Journal of Fluid Mechanics

    Extended Squire's transformation and its consequences for transient growth in a confined shear flow

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    International audienceThe classical Squire transformation is extended to the entire eigenfunction structure of both Orr-Sommerfeld and Squire modes. For arbitrary Reynolds numbers Re, this transformation allows the solution of the initial-value problem for an arbitrary three-dimensional (3D) disturbance via a two-dimensional (2D) initial-value problem at a smaller Reynolds number Re-2D. Its implications for the transient growth of arbitrary 3D disturbances is studied. Using the Squire transformation, the general solution of the initial-value problem is shown to predict large-Reynolds-number scaling for the optimal gain at all optimization times t with t/Re finite or large. This result is an extension of the well-known scaling laws first obtained by Gustavsson (J. Fluid Mech., vol. 224, 1991, pp. 241-260) and Reddy & Henningson (J. Fluid Mech., vol. 252, 1993, pp. 209-238) for arbitrary alpha Re, where alpha is the streamwise wavenumber. The Squire transformation is also extended to the adjoint problem and, hence, the adjoint Orr-Sommerfeld and Squire modes. It is, thus, demonstrated that the long-time optimal growth of 3D perturbations as given by the exponential growth (or decay) of the leading eigenmode times an extra gain representing its receptivity, may be decomposed as a product of the gains arising from purely 2D mechanisms and an analytical contribution representing 3D growth mechanisms equal to 1 + (beta Re/Re-2D)(2) g where beta is the spanwise wavenumber and g is a known expression. For example, when the leading eigenmode is an Orr Sommerfeld mode, it is given by the product of respective gains from the 2D On mechanism and an analytical expression representing the 3D lift-up mechanism. Whereas if the leading eigenmode is a Squire mode, the extra gain is shown to be solely due to the 3D lift-up mechanism. Direct numerical solutions of the optimal gain for plane Poiseuille and plane Couette flow confirm the novel predictions of the Squire transformation extended to the initial-value problem. These results are also extended to confined shear flows in the presence of a temperature gradient

    Liquid inertia versus bubble cloud buoyancy in circular plunging jet experiments

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    When a liquid jet plunges into a pool, it can generate a bubble-laden jet flow underneath the surface. This common and simple phenomenon is investigated experimentally for circular jets to illustrate and quantify the role played by the net gas/liquid void fraction on the maximum bubble penetration depth. It is first shown that an increase in either the impact diameter or the jet fall height to diameter ratio at constant impact momentum leads to a reduction in the bubble cloud size. By systematically measuring the local void fraction using optical probes in the biphasic jet, it is then demonstrated that this effect is a direct consequence of the increase in the air content within the cloud. A simple momentum balance model, including only inertia and the buoyancy force, is shown to predict the bubble cloud depth without any fitting parameters. Finally, a Froude number based on the bubble terminal velocity, the cloud depth, and also the net void fraction is introduced to propose a simple criterion for the threshold between the inertia-dominated and buoyancy-dominated regimes.Comment: As of 16th of November 2023, it is accepted for publication in JF

    Vortex-forced-oscillations of thin flexible plates

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    Fluid-structure interaction of a slender flexible cantilevered-element and vortices in an otherwise steady flow is considered here by investigating the dynamics of thin low-density polyethylene sheets subject to periodic forcing due to B\'enard-K\`arm\`an vortices in a 22-meter long narrow water channel. The vortex shedding frequency fvf_v is varied via the mean flow speed U0U_0 and the cylinder diameter d0=10d_0 = 10, 2020 and 4040 mm, while the structures' bending resistance is properly controlled via its Young's modulus EE, thickness ebe_b and length LbL_b. Thereby, it is first shown that the non-dimensional time-averaged sheet deflection, namely, the sheet \textit{reconfiguration} hˉb/LbCyV/2\bar{h}_b/L_b \sim C_y^{\mathcal{V}/2} and also, the time-averaged \textit{drag force} FˉdU02+V\bar{F}_d \propto U_0^{2+\mathcal{V}}, where V0\mathcal{V} \leq 0 is the well-known Vogel number for flexible structures in a steady flow and Cy=12(Cd12ρU02/E)(Lb3/eb3)C_y = 12 \left({C_d \frac{1}{2} \rho U_0^2}/{E}\right) \left({ L_b^3/}{e_b^3} \right) is the Cauchy number comparing the relative magnitude of the profile drag force over a typical elastic restoring force, if the sheet were rigid. Measurements and a simple model based on torsional-spring-mounted flat plate illustrate that the tip amplitude δb\delta_b is not only directly proportional to the characteristic size of the eddies, say dvd_v, but also to the sheet mechanical properties and the vortex flow characteristics such that δb/dvCy(1+V)/2U0/fvdv\delta_b/d_v \sim C_y^{(1+\mathcal{V})/2} \sqrt{U_0/f_v d_v}. Furthermore, a rich phenomenology of structural dynamics including vortex-forced-vibration, lock-in with the sheet natural frequency, flow-induced vibration due to the sheet wake, multiple-frequency and modal response is reported

    Vortices catapult droplets in atomization

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    International audienceA droplet ejection mechanism in planar two-phase mixing layers is examined. Any disturbance on the gas-liquid interface grows into a Kelvin-Helmholtz wave, and the wave crest forms a thin liquid film that flaps as the wave grows downstream. Increasing the gas speed, it is observed that the film breaks up into droplets which are eventually thrown into the gas stream at large angles. In a flow where most of the momentum is in the horizontal direction, it is surprising to observe these large ejection angles. Our experiments and simulations show that a recirculation region grows downstream of the wave and leads to vortex shedding similar to the wake of a backward-facing step. The ejection mechanism results from the interaction between the liquid film and the vortex shedding sequence: a recirculation zone appears in the wake of the wave and a liquid film emerges from the wave crest; the recirculation region detaches into a vortex and the gas flow over the wave momentarily reattaches due to the departure of the vortex; this reattached flow pushes the liquid film down; by now, a new recirculation vortex is being created in the wake of the wave--just where the liquid film is now located; the liquid film is blown up from below by the newly formed recirculation vortex in a manner similar to a bag-breakup event; the resulting droplets are catapulted by the recirculation vortex

    LA CROISSANCE TRANSITOIRE DANS LES ÉCOULEMENTS DE RAYLEIGH-BÉNARD-POISEUILLE/COUETTE

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    OPTIMAL GROWTH MECHANISMS IN WALL-BOUNDED SHEAR FLOWS, IN PARTICULAR, PLANE COUETTE AND PLANE POISEUILLE FLOW, WITH AND WITHOUT A DESTABILIZING WALL-NORMAL TEMPERATURE GRADIENT ARE STUDIED EXTENSIVELY. IN THE CASE WITH A CROSS-STREAM TEMPERATURE GRADIENT IN A BOUSSINESQ FLUID, A COMPREHENSIVE NON-MODAL STABILITY ANALYSIS IS PERFORMED OVER VARIOUS REYNOLDS, RAYLEIGH AND PRANDTL NUMBERS. THE SCALING LAWS PERTAINING TO TRANSIENT GROWTH IN PURE SHEAR FLOWS ARE SHOWN TO HOLD EVEN IN THE PRESENCE OF A DESTABILIZING TEMPERATURE GRADIENT. THE LIFT-UP EFFECT REMAINS THE PREDOMINANT TRANSIENT GROWTH MECHANISM. THE CLASSICAL INVISCID LIFT-UP MECHANISM CHARACTERIZES THE SHORT-TIME BEHAVIOR WHEREAS THE RAYLEIGH-BÉNARD EIGENMODE WITHOUT ITS STREAMWISE VELOCITY COMPONENT CHARACTERIZES THE LONG-TIME BEHAVIOR. THE SQUIRE TRANSFORMATION IS EXTENDED TO PROVIDE NEW INSIGHTS ON THE OPTIMAL GROWTH OF ARBITRARY 3D DISTURBANCES IN PARALLEL SHEAR FLOWS BOUNDED IN THE CROSS-STREAM DIRECTION. IT ALSO PERMITS TO DEMONSTRATE THAT THE LONG-TIME OPTIMAL GROWTH FOR PERTURBATIONS OF ARBITRARY WAVENUMBERS MAY BE DECOMPOSED AS A PRODUCT OF THE RESPECTIVE GAINS ARISING FROM THE 2D ORR-MECHANISM AND THE LIFT-UP MECHANISM. THIS ASYMPTOTIC SOLUTION IS SHOWN TO DESCRIBE THE LONG-TIME AND EVEN THE INTERMEDIATE-TIME DYNAMICS OF THE OPTIMAL DISTURBANCES AND PROVIDES A GOOD ESTIMATE OF THE MAXIMUM OPTIMAL GAIN AT ALL TIME.LES MÉCANISMES DE CROISSANCE OPTIMALE DANS DES ÉCOULEMENTS DE CISAILLEMENT CONFINES, EN PARTICULIER LES ÉCOULEMENTS DE COUETTE PLAN ET POISEUILLE PLAN, LORSQU'ILS SONT SOUMIS OU NON À UN GRADIENT DE TEMPÉRATURE DÉSTABILISANT NORMAL À LA PAROI SONT ÉTUDIÉS EN DÉTAIL. DANS LE CAS D'UN FLUIDE DE BOUSSINESQ SOUMIS À UN GRADIENT DE TEMPÉRATURE TRANSVERSE, UNE ANALYSE EXHAUSTIVE DE STABILITÉ NON MODALE EST EFFECTUÉE POUR DIFFÉRENTS NOMBRES DE REYNOLDS, DE RAYLEIGH ET DE PRANDTL. ON MONTRE QUE LES LOIS D'ÉCHELLE RELATIVES À LA CROISSANCE TRANSITOIRE DANS DES ÉCOULEMENTS CISAILLES PURS SONT ROBUSTES, Y COMPRIS EN PRÉSENCE D'UN GRADIENT DE TEMPÉRATURE DÉSTABILISANT. L'EFFET DE ''LIFT-UP" RESTE LE MÉCANISME PRÉDOMINANT DE CROISSANCE TRANSITOIRE. LE MÉCANISME DE ''LIFT-UP" NON VISQUEUX CLASSIQUE CARACTÉRISE LE COMPORTEMENT AUX TEMPS COURTS ALORS QUE LE MODE PROPRE DE RAYLEIGH-BÉNARD SANS SA COMPOSANTE DE VITESSE LONGITUDINALE CARACTÉRISE LE COMPORTEMENT AUX TEMPS LONGS. LA COURBE DE GAIN OPTIMAL EST AINSI DÉCRITE ET INTERPRÉTÉE ENTIÈREMENT. DANS LE CAS D'ÉCOULEMENTS CISAILLES PURS, LE RÔLE DE TRANSFORMATION DE SQUIRE EST ÉTENDUE À LA CROISSANCE TRANSITOIRE OPTIMALE D'UNE PERTURBATION ARBITRAIRE 3D DANS LE CAS D'ÉCOULEMENTS CISAILLES PARALLÈLES D'EXTENSION TRANSVERSE FINIE. CELA PERMET AUSSI DE DÉMONTRER QUE LES CROISSANCES OPTIMALES AUX TEMPS LONGS POUR DES PERTURBATIONS DE NOMBRE D'ONDE ARBITRAIRES PEUVENT ÊTRE DÉCOMPOSÉES COMME UN PRODUIT DES GAINS RESPECTIFS RÉSULTANT DU MÉCANISME D'ORR 2D ET DU MÉCANISME DE " LIFT-UP "

    Nurse Selection Project - digest of work

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    SIGLEAvailable from British Library Document Supply Centre- DSC:q94/22829 / BLDSC - British Library Document Supply CentreGBUnited Kingdo
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