Non-isothermal flow diagnostics using microencapsulated cholesteric particles

The temperature and the flow field of thermo-convective liquid flows are visualized using cholesteric liquid crystal material as tracer particles. This type of tracers offers the scientifically valuable feature of measuring the flow and the temperature field simultaneously. Three thermoconvective flow configurations have been investigated successfully using liquid crystals. The results are discussed in some detail. It turns out that the liquid crystal technique is a valuable tool for thermo-convective liquid flow analysis.     

Unsteady flow in rotating drums using laser Doppler velocimetry

Non-destructive measurements by laser Doppler velocimetry is employed to study unsteady flow in a hollow drum filled with liquid. The drum is suddenly accelerated from rest or is suddenly decelerated from a steady rotation to rest. Pure water and glycerin-water mixtures are used as the test liquid in which polyethylenelatex particles are mixed as the light scattering tracer. The boundary layer formation, the time history of velocity, momentum and kinetic energy of the liquid, the wall-to-fluid force transfer, and the transient response time are determined. Also determined are the effects of side walls and fluid viscosity on the transient flow response. Of importance is the disclosure of Ekman layer instability near the inner radial wall of the test drum. It is actuated by the centripetal acceleration-induced buoyancy force.List of symbols A wetted surface area of test drum, cm² - a reciprocal of characteristic velocity, = t _sH, s/cm - B width of test drum, cm - b axial coordinate of test drum, cm - D diameter of test drum, cm; D ₁, inner diameter; D ₂, outer diameter - d diameter of laser beam, mm - d _p particle diameter, mm - E kinetic energy of liquid, kg · cm²/s²; E _s, steady value - F force transferred from drum walls to liquid, N - f focal length of lens, mm - G one-half of spacing between two parallel split beams, Fig. 1 - H characteristic length of test drum, cm; = V/A - M momentum of liquid, kg·cm/s; M _s, steady value - m mass of control volume, kg - r radial coordinate of test drum, cm - S fringe spacing, mm - t time, s - t _p time for particle to travel through fringe spacing, s - t _s transient time, s - u liquid velocity, cm/s - V liquid volume in test drum, cm³ - V _s effective volume of sample volume, mm³ - v velocity of tracer particle, cm/s; = S/t - W waist diameter of parabola in Fig. 2, mm - (x, y, z) coordinates for paraboloid in Fig. 2, mm - crossing angle of splitting beams, degrees - wavelength of laser length, cm - v kinematic viscosity, cm²/s - liquid density, kg/cm³ - Doppler frequency, l/s - s at steady state - 1 outer - 2 inner On leave from the Dept. of Mechanical Engineering, Musashi Institute of Technology, Tokyo, Japan     

Unsteady flow through screens

Summary Reflected and transmitted pressure waves take place when an incident pressure wave reaches a screen placed in a duct and crossed by a previous steady flow. The thickness of the screen is assumed to be negligible and essure losses through it in the quasi steady flow, which takes place after the passage of the incident pressure wave, are assumed be steady flow ones. The strength of reflected and transmitted pressure waves is related to the strength of the incident wave, to the porosity of the screen and to the previous flow through it. Subsonic and just supersonic quasi steady flow inside the screen are considered. Five commercial screens have been tested with incident shock waves and the experimental results have been compared with the theoretical ones: the agreement is quite satisfactory.

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Sommario L'interazione di un'onda di pressione con una rete intubata attraversata da un flusso preesistente produce un'onda riflessa ed una trasmessa. Si presenta un modello teorico basato essenzialmente sulle potesi che lo spessore della rete sia trascurabile e che le perdite carico attraverso di essa, nel flusso quasi stazionario indotto dalla suddetta interazione, coincidano con quelle proprie di un oto permanente. Si analizza il caso di flusso indotto nella rete ia subsonico che sonico. Si eseguono prove sperimentali su cinque reti di diverse porosità differenti condizioni di flusso, e si verifica l'attendibilità del odello teorico proposto.

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The present work has been supported by the “Consiglio Nazionale delle Ricerche” (C.N.R.) under Contract no. 115.4075.69.01220.

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The suffixes “u” and “d” pertain to the conditions upstream and downstream of the screen with reference to the flow through it. The suffix “j” refers to the region “j” of the wave diagrams in Fig. 1.     

Unsteady unidirectional micropolar fluid flow

This paper considers the unsteady unidirectional flow of a micropolar fluid, produced by the sudden application of an arbitrary time dependent pressure gradient, between two parallel plates. The no-slip and the no-spin boundary conditions are used. Exact solutions for the velocity and microrotation distributions are obtained based on the use of the complex inversion formula of Laplace transform. The solution of the problem is also considered if the upper boundary of the flow is a free surface. The particular cases of a constant and a harmonically oscillating pressure gradient are then examined and some numerical results are illustrated graphically.     

Unsteady supersonic flow over an oscillatory aerofoil using a second-order TVD scheme

The unsteady flow over an oscillatory NACA0012 aerofoil has been simulated by the calculation with Euler equations. The equations are discretized by an implicit Euler in time, and a second-order space-accurate TVD scheme based on flux vector splitting with van Leer's limiter. Modified eigenvalues are proposed to overcome the slope discontinuities of split eigenvalues at Mach = 0·0 and ± 1·0, and to generate a bow shock in front of the aerofoil. A moving grid system around the aerofoil is generated by Sorenson's boundary fitted co-ordinates for each time step. The calculations have been done for two angles of attack θ = 5·0° sin (ωt) and θ = 3·0° + 3·0° sin (ωt) for the free-stream Mach numbers 2·0 and 3·0. The results show that pressure and Mach cells flow along characteristic lines. To examine unsteady effects, the responses of wall pressure and normal force coefficients are analysed by a Fourier series expansion.     

Unsteady flow of viscoelastic fluid between two cylinders using fractional Maxwell model

The unsteady flow of an incompressible fractional Maxwell fluid between two infinite coaxial cylinders is studied by means of integral transforms.The motion of the fluid is due to the inner cylinder that applies a time dependent torsional shear to the fluid.The exact solutions for velocity and shear stress are presented in series form in terms of some generalized functions.They can easily be particularized to give similar solutions for Maxwell and Newtonian fluids.Finally,the influence of pertinent parameters on the fluid motion,as well as a comparison between models,is highlighted by graphical illustrations.     

Holographic velocimetry for flow diagnostics

Currently, there are a number of flow diagnostic tools available for the evaluation of fluid dynamic systems. In spite of its great potential, holographic velocimetry is one technique which has not been widely used. It does, however, have great potential in this area due to its inherent three-dimensionality. As demonstrated in this study of fully developed turbulent flow in a pipe, full three-dimensional mapping can be achieved at any instant in a flow cycle. Comparisons of holographic results with analytical predictions and laser-Doppler-anemometry (LDA) measurements demonstrate the accuracy of the technique as well as some of its advantages and disadvantages relative to LDA. Although relatively poor spatial resolution is obtained, the fact that holographic velocimetry is both an instantaneous and full volume measuring tool makes it useful for a range of complex and high-speed flow-measurement applications.     

Unsteady flow over a rough bottom

The unsteady motion of an ideal incompressible fluid with a free surface, developing from a state of rest, is considered. The flow is assumed to be irrotational, continuous and two-dimensional; it may be the result either of an initial disturbance of the free boundary or of a given boundary pressure distribution. The rigid boundaries of the flow region are fixed, and the free surface does not cross them at any time during the motion. The fluid is located in a uniform gravity force field and there is no surface tension. A method which in the case of localized roughness of the bottom makes it possible to find the shape of the free surface at any moment of time with predetermined accuracy is proposed. The method involves reducing the initial linear problem to a Volterra integral equation of the second kind, the kernel of this equation being a nonlocal operator. This operator has a smoothing effect, which makes it possible to reduce the solution of the initial problem to the solution of an infinite, perfect lyregular system of Volterra integral equations for a denumerable set of auxiliary functions.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 111–119, November–December, 1989.The author is grateful to I. V. Sturova and B. E. Protopopov for useful discussions and criticism.     

Unsteady saturated-unsaturated flow to horizontal drains

On irrigated ground with poor natural drainage, artificial drainage is used to prevent secondary salinization and swamping. The calculation of the drainage parameters requires the solution of problems of saturated-unsatated flow in the region between the drains [1–6]. The influence of the motion in the unsaturated region on the total flow of ground water is most important when the water-saturated region is thin and especially in the case of finely grained soil. If the capillary border intersects the surface of the ground and there is an alternation of the processes of infiltration, redistribution, and evaporation of moisture, rapid oscillations in the ground water level are possible. Under these conditions, calculation of the drainage parameters using hydraulic models [7], which do not take into account motion in the region of incomplete saturation, is made difficult by the need to specify the coefficient which measures the incompleteness of saturation, and also the rates of flow between the aeration region and the ground water. The present paper gives the mathematical formulation, an algorithm for numerical solution, and examples of calculations for a two-dimensional problem of unsteady joint flow of ground water and soil moisture.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 5, pp. 81–87, September–October, 1981.     

Unsteady behavior of back-facing step flow

In this paper, a contribution to the study of the unsteady behavior of a back-facing step flow is reported. The main interest is devoted to low-frequency motions. A probe for skin friction measurements is employed to acquire time histories from the step to downstream the reattachment region. Signals are analyzed in the physical space and in the frequency domain. The obtained results, associated with flow visualization in a companion experiment in water, support a model of cyclic motion of growing and successive breakdown of the secondary recirculating bubble. The frequency of this quasi-periodic motion is comparable to the flapping frequency of the whole separated region, reported in the literature. Received: 14 February 2000/Accepted: 5 September 2000     

Unsteady transonic flow around double-wedge profiles

A double-wedge with a relative thickness d/c > 0.15 forms a vortex street in its wake. This was investigated experimentally in the Mach number range of 0.4 to 0.75. The strength and the frequency of the pressure fluctuations which are produced by the vortices, were measured on the surface of the wedge for different chord length and relative thickness, both in chord- and spanwise direction. The density fluctuations around the profile and in the wake were measured with a Mach-Zehnder interferometer and a schlieren system. Attention was focussed on the question concerning to what extent unsteady flows are affected by wall interferences.     

Unsteady flow around impacting bluff bodies

The flow resulting from the collision without rebound of generic bluff bodies with a wall in a still viscous fluid is investigated both computationally and experimentally. Emphasis is on the case of a circular cylinder impact (two-dimensional geometry), but comparisons with the flow generated by the impact of a sphere (axisymmetric geometry) are included. For normal cylinder impacts, the two counter-rotating vortices forming behind the body during its motion continue their trajectory towards the wall after the collision, leading to the generation of opposite-signed secondary vorticity at the cylinder and wall surfaces. Secondary vortices forming from this vorticity at higher Reynolds numbers exhibit a short-wavelength three-dimensional instability. Comparison with the sphere impact reveals significant differences in the scales of the vortices after the collision, due to the additional vortex stretching acting in the axisymmetric geometry. This leads to a delay in the onset of three-dimensionality and to a different instability mechanism. Oblique cylinder impacts are also considered. For increasing impact angles, the wall effect is gradually reduced on one side of the cylinder, which favours the roll-up of the secondary vorticity and increases the rebound height of the vortex system.     

Unsteady flow in a circular sector duct

Analytic solutions for the unsteady flow in a circular sector duct are found using series sums of Bessel integrals. For starting flow due to a step pressure gradient, the velocity profile is initially flat, then approaches the rounded steady state shape in a time scale proportional to the square of opening angle of the sector. For oscillatory flow, the velocity is quasi-steady for low frequencies, but shows “annular effect” at large frequencies. Increased opening angle increases the amplitude and the phase lag. In all cases, the shear stress at the apex is zero for acute sector angles but becomes infinite for obtuse sector angles.     

Unsteady elastico-viscous flow in a curved pipe

Summary An analysis is presented of the flow of an elasticoviscous liquid in a pipe of circular cross-section, coiled in a circle oflarge radiusR, under the influence of a pressure gradient oscillating (about a zero mean) with frequencyn. Of particular interest is the secondary flow set up in the cross-section of the pipe due to centrifugal effects. For sufficiently small values ofn, it is found that the flow pattern approaches that which would be produced by a steady pressure gradient having the same instantaneous value (Thomas andWalters 1963), and of the type that one would be led to expect by centrifugal effects. For large values ofn, the flow in the interior of the pipe, away from the wall, is spectacularly reversed, flow now being directed towards the centre of curvature, elasticity having the effect of reducing the critical (high) frequencyn = n _c which onsets flow reversal.

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Zusammenfassung Eine Analyse der Strömung einer elasto-viskosen Flüssigkeit in einer Röhre von rundem Querschnitt, die in einem Kreis mit einemgroßen RadiusR gewunden ist, wird unter dem Einfluß eines Druckgradienten, der mit der Frequenzn oszilliert (um einen Nulldurchschnitt), dargestellt. Von besonderem Interesse ist die Sekundärströmung, die in dem Querschnitt der Röhre unter dem Einfluß der Zentrifugalwirkungen entsteht. Für genügend kleine Werte vonn wird herausgefunden, daß das Strömungsbild sich demjenigen annähert, das von einem stationären Druckgradienten erzeugt werden würde, der denselben augenblicklichen Wert besitzt (Thomas andWalters 1963) und dem Typus angehört, den man aufgrund der Zentrifugalwirkungen erwarten würde. Für große Werte vonn wird die Strömung im Inneren der Röhre, d. h. von den Rändern entfernt, in spektakulärer Weise umgekehrt; jetzt wird die Strömung zum Krümmungsmittelpunkt hin gerichtet, und die Elastizität hat die Wirkung, die kritische (hohe) Frequenzn = n _c zu reduzieren, bei der die Strömungsumkehr beginnt.

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With 2 figures