Optical co-ordinates in general relativity 2 — the problem of distance

Summary Let denote the congruence of null geodesics associated with a given optical observer inV ₄. We prove that determines a unique collection of vector fieldsM₍₎ ( =1, 2, 3) and ₍₀₎ overV ₄, satisfying a weak version of Killing's conditions.This allows a natural interpretation of these fields as the infinitesimal generators of spatial rotations and temporal translation relative to the given observer. We prove also that the definition of the fieldsM₍₎ and ₍₀₎ is mathematically equivalent to the choice of a distinguished affine parameter f along the curves of, playing the role of a retarded distance from the observer.The relation between f and other possible definitions of distance is discussed.

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Sommario Sia la congruenza di geodetiche nulle associata ad un osservatore ottico assegnato nello spazio-tempoV ₄. Dimostriamo che determina un'unica collezione di campi vettorialiM₍₎ ( =1, 2, 3) e ₍₀₎ inV ₄ che soddisfano una versione in forma debole delle equazioni di Killing. Ciò suggerisce una naturale interpretazione di questi campi come generatori infinitesimi di rotazioni spaziali e traslazioni temporali relative all'osservatore assegnato. Dimostriamo anche che la definizione dei campiM₍₎, ₍₀₎ è matematicamente equivalente alla scelta di un parametro affine privilegiato f lungo le curve di, che gioca il ruolo di distanza ritardata dall'osservatore. Successivamente si esaminano i legami tra f ed altre possibili definizioni di distanza in grande.

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Work performed in the sphere of activity of: Gruppo Nazionale per la Fisica Matematica del CNR.     

Einfluß der Beheizungsart auf den Wärmeübergang im horizontalen Verdampferrohr

Zusammenfassung Durch die Phasenverteilung von Flüssigkeit und Dampf ergeben sich im horizontalen Verdampferrohr i.a. unterschiedliche lokale Wärmeübergangskoeffizienten (WÜK) am Rohrumfang. Die beiden technisch vorkommenden Randbedingungen — konstante Wärmestromdichte und konstante WandemperaturT _W am Rohrinnendurchmesser — können unterschiedliche Auswirkungen auf umfangsgemittelte WÜK haben. Während bei konstanter aufgeprägter Wärmestromdichte ein interner Transport der zu übertragenden Wärmemenge durch die Wärmeleitung der Wand erfolgen kann, ist dies beiT _W =konst. nicht möglich. Die Ergebnisse zeigen, daß sich der umfangsgemittelte WÜK bei konstanter Wärmestromdichte gegenüber dem Wert bei konstanter Wandtemperatur verringert. Dies ist jedoch nur dann der Fall, wenn der Rohrumfang unvollständig benetzt ist. Dabei hängt die Verminderung des umfangsgemittelten WÜK stark vom Wärmeleitvermögen der Wand, s, ab ( Wärmeleitfähigkeit,s Wandstärke). Es wurde festgestellt, daß die Verminderung sowohol aus der höheren Wandtemperatur am Rohrscheitel als auch aus der Änderung des benetzten Umfangs resultiert, da dann der Anteil des Rohrumfangs mit schlechtem Wärmeübergang vergrößert wird.

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Effect of thermal boundary conditions on heat transfer in a horizontal evaporator tube

As a result of the non uniform phase distribution of liquid and vapour local heat transfer coefficients vary considerably along the circumference in a horizontal evaporator tube. It was expected that both modes of heating, uniform heat flux ( = const) and uniform inside wall temperature (T _W =const), lead to different circumferential averaged heat transfer coefficients (HTC). The experiments show that the circumferential averaged HTC is lower in the case of uniform heat flux compared to the value of uniform wall temperature if the perimeter of the tube is only partly wetted. However, the reduction is affected by circumferential heat conduction. This reduction is a result of both, the higher wall temperature on the top of the tube and the reduction of the wetted perimeter.

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Formelzeichen a Verhältnis von -Werten - c _p spezifische Wärmekapazität - C _F Faktor - d Innendurchmesser - g Fallbeschleunigung - h _v spezifische Verdampfungsenthalpie - Massenstromdichte - M Rippenkenngröße - n Exponent der Wärmestromdichte - Nu Nusselt-Zahl - p Druck - p _k Kritischer Druck - p* reduzierter Druck (p/p _k ) - Pr _L Prandtl-Zahl Flüssigkeit ( c _p /) - Pr _G Prandtl-Zahl Dampf ( c _p /) - Wärmestromdichte - r Radius - Re Reynolds-Zahl - R _p Glättungstiefe nach DIN 4762 - s Wandstärke - T Temperatur - Strömungsdampfgehalt - z Koordinate in Strömungsrichtung - Wärmeübergangskoeffizient - Differenz - Dampfvolumenanteil - dynamische Viskosität - Faktor - Wärmeleitfähigkeit - Druckverlustbeiwert - Dichte - Oberflächenspannung - normierter unbenetzter Bogen - Zentriwinkel - unbenetzter Bogen - Funktion - Faktor Indizes B Blasensieden - G Dampf - G0 gesamte Massenstromdichte als Dampf - k konvektives Strömungssieden - kr kritische Größe - L Flüssigkeit - Lb mit Flüssigkeit benetzt - L0 gesamte Massenstromdichte als Flüssigkeit - s Siedezustand - W Wand - gesättigte Flüssigkeit - gesättigter Dampf - – Mittelwert Herrn Prof. Dr.-Ing. Dr. h.c./INPL E.-U. Schlünder zum 60. Geburtstag gewidmet     

General expressions for unsteady forces in a lattice of profiles

A large number of studies have been devoted to the unsteady flow of a viscid incompressible fluid past a lattice of thin profiles and the determination of the resulting aerodynamic forces and moments. For example, in the particular case of the motion of a lattice with stagger with zero phase shift of the oscillations between neighboring profiles, Haskind [1] determined the unsteady lift force and moment. Popescu [2] suggested expressions for the force and moment in the case when =0 and =0, using the method of conformal mapping. Samoilovich [3] obtained equations for the unsteady lift force and moment by the method of the acceleration potential for phase shift =0 and = of the oscillations between neighboring profiles. Musatov [4] used an electronic digital computer to calculate the overall unsteady aerodynamic characteristics of a grid by the vortex method, taking into account the amplitude of the oscillations and the initial circulation for =m (m1). Gorelov [5] determined the coefficients of the over-all unsteady aerodynamic force and moment of a profile in a lattice with the stagger and any value of =m. He used a method based on the unsteady flow past an isolated profile with subsequent account for the interference of the profiles in the lattice.In the following we find general expressions for the unsteady lift force and moment acting on a lattice moving in an incompressible fluid with the constant velocity U. These formulas generalize the known formulas for the isolated profile [6]. The profiles of a staggered grid (Section 1) are considered to be thin and slightly curved, and perform oscillations with a phase shift of the oscillations between neighboring profiles. The method of separation of singularities is used to obtain the solution in closed form. The coefficients of the expansion of the complex velocity in a series in the derivatives of a function are calculated. An integral equation relative to the unknown tangential velocity component in the wake is derived (Section 2), and its analytic solution is given (Section 3). For =0 the solution coincides with the solution obtained earlier in [7]. Expressions are obtained for the forces and moments (Section 4) in the form of four terms. The first two terms determine the force and moment for motion with constant circulation, and the last two determine these characteristics for motion with variable circulation. The suction force acting at the leading edges of the profiles is found in a general form. Particular cases of closely and widely spaced lattices are considered. Computational results are presented.     

Evaluation of the dynamic-mechanical properties of solids from a cooperative model for stress relaxation

For many solid materials the stress relaxation process obeys the universal relationF = – (d/d lnt)_max = (0.1 ± 0.01) ( ₀ — _i ), regardless of the structure of the material. Here denotes the stress,t the time, ₀ the initial stress of the experiment and _i the internal stress. A cooperative model accounting for the similarity in relaxation behaviour between different materials was developed earlier. Since this model has a spectral character, the concepts of linear viscoelasticity are used here to evaluate the corresponding prediction of the dynamic mechanical properties, i.e. the frequency dependence of the storageE () and lossE () moduli. Useful numerical approximations ofE () andE () are also evaluated. It is noted that the universal relation in stress relaxation had a counterpart in the frequency dependence ofE (). The theoretical prediction of the loss factor for high-density polyethylene is compared with experimental results. The agreement is good.     

A rotating hot-wire technique for spatial sampling of disturbed and manipulated duct flows

The documentation and control of flow disturbances downstream of various open inlet contractions was the primary focus with which to evaluate a spatial sampling technique. An X-wire probe was rotated about the center of a cylindrical test section at a radius equal to one-half that of the test section. This provided quasi-instantaneous multi-point measurements of the streamwise and azimuthal components of the velocity to investigate the temporal and spatial characteristics of the flowfield downstream of various contractions. The extent to which a particular contraction is effective in controlling ingested flow disturbances was investigated by artificially introducing disturbances upstream of the contractions. Spatial as well as temporal mappings of various quantities are presented for the streamwise and azimuthal components of the velocity. It was found that the control of upstream disturbances is highly dependent on the inlet contraction; for example, reduction of blade passing frequency noise in the ground testing of jet engines should be achieved with the proper choice of inlet configurations.List of symbols K _uv correlation coefficient= - P percentage of time that an azimuthal fluctuating velocity derivative dv/d is found - U streamwise velocity component U=U (, t) - V azimuthal or tangential velocity component due to flow and probe rotation V=V (, t) - mean value of streamwise velocity component - U _m resultant velocity from and - mean value of azimuthal velocity component induced by rotation - u fluctuating streamwise component of velocity u=u(, t) - v fluctuating azimuthal component of velocity v = v (, t) - u phase-averaged fluctuating streamwise component of velocity u=u(0) - v phase-averaged fluctuating azimuthal component of velocity v=v() - û average of phase-averaged fluctuating streamwise component of velocity (u()) over cases I-1, II-1 and III-1 û = û() - average of phase-averaged fluctuating azimuthal component of velocity (v()) over cases I-1, II-1 and III-1 - u fluctuating streamwise component of velocity corrected for non-uniformity of probe rotation and/or phase-related vibration u = u(0, t) - v fluctuating azimuthal component of velocity corrected for non-uniformity or probe rotation and/or phase-related vibration v=v (, t) - u ² rms value of corrected fluctuating streamwise component of velocity - rms value of corrected fluctuating azimuthal component of velocity - phase or azimuthal position of X-probe     

Diophantine conditions and K.A.M. estimates for the Siegel theorem in CN

Summary We give a simple proof of Siegel's linearization theorem of germs of complex analytic diffeomorphisms of ^N near a fixed point. The proof leads to realistic bounds when applied to polynomial maps of . Numerical estimates, based on rigorous arguments, are also given. For non-quadratic mappings we find that winding numbers different from the golden mean might determine the stochastic transition.

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Sommario Viene data una dimostrazione semplice del teorema di Siegel sulla linearizzazione di germi di diffeomorfismi analitici di ^N vicino a un punto fisso. La dimostrazione conduce a stime realistiche quando viene applicata a mappe polinomiali di . Vengono date inoltre delle stime numeriche, che si fondano su argomenti rigorosi. Si trova che per mappe non quadratiche numeri di notazione diversi dal numero d'oro potrebbero determinare la transizione al caos.

     

Steady rotatory flow of Bingham material between two concentric spheres

Summary Steady flow of Bingham material between two concentric rotating spheres has been investigated taking into account the constitutive equations given by Oldroyd. Motions in the elastic as well as in the flow region have been discussed. A critical value of the Bingham number has been found below which the flow takes place in the whole region and above which the elastic and flow regions occur side by side.Nomenclature r, , space co-ordinates - u _r ,u ,u velocity components - density - modulus of rigidity (constant) - bulk modulus - e _ii , the dilatation - ₁ coefficient of viscosity (constant) - e _ik strain tensor - d _ik rate of strain tensor - p _ik stress tensor primes denote deviatoric components of tensors, e.g. - p _ik p _ik +p _k ⁱ , p=–1/3p _ii - yield value (constant) - D/Dt materiaal derivative with regard to time following the particle - R ₁ radius of the inner sphere - R ₂ radius of the outer sphere - R radius of the yield surface (spherical) - ₁ velocity of the inner sphere - B Bingham number     

Existence theorem for a minimum problem with free discontinuity set

We study the variational problem Where is an open set in ⁿ ,n2gL ^q () L (), 1q<+, O<, <+ andH _n–1 is the (n–1)-dimensional Hausdorff Measure.     

On surface waves in generalized thermoelasticity

Knowles' representation theorem for harmonically time-dependent free surface waves on a homogeneous, isotropic elastic half-space is extended to include harmonically time-dependent free processes for thermoelastic surface waves in generalized thermoelasticity of Lord and Shulman and of Green and Lindsay.r , , r , , .This work was done when author was unemployed.     

Asymptotic analysis of equilibrium states for rotating turbulent flows

The equilibrium states of homogeneous turbulence simultaneously subjected to a mean velocity gradient and a rotation are examined by using asymptotic analysis. The present work is concerned with the asymptotic behavior of quantities such as the turbulent kinetic energy and its dissipation rate associated with the fixed point (/kS)=0, whereS is the shear rate. The classical form of the model transport equation for (Hanjalic and Launder, 1972) is used. The present analysis shows that, asymptotically, the turbulent kinetic energy (a) undergoes a power-law decay with time for (P/)<1, (b) is independent of time for (P/)=1, (c) undergoes a power-law growth with time for 1<(P/)<(C ₂–1), and (d) is represented by an exponential law versus time for (P/)=(C ₂–1)/(C ₁–1) and (/kS)>0 whereP is the production rate. For the commonly used second-order models the equilibrium solutions forP/,II, andIII (whereII andIII are respectively the second and third invariants of the anisotropy tensor) depend on the rotation number when (P/kS)=(/kS)=0. The variation of (P/kS) andII versusR given by the second-order model of Yakhot and Orzag are compared with results of Rapid Distortion Theory corrected for decay (Townsend, 1970).     

Filament stretching equation in Lagrangian coordinates

The general integral of the very simple equation ^21/n/() was found to describe the cross sectional area of filaments of isothermal power law fluids while in transient stretching where is time and is the initial location of fluid molecules at time = 0 given as the distance from a reference point fixed in space. Any such stretching transient given as a solution of the above equation is physically realizable subject to the restrictions > 0 and/ < 0.     

Critical phenomena and waves in gas-liquid systems

The results of the hydraulic studies of gas-liquid media, wave processes in two-phase media and critical phenomena are described. Some methodological foundations to describe these media and methods to obtain the basic similarity criteria for the hydraulics and gas-dynamics of bubble suspensions are discussed. A detailed consideration is given for the phase transition processes on interfaces and the interface stability. A relation has been revealed between the wave and critical phenomena in two-phase systems.Nomenclature a thermal diffusivity - Ar Archimedes number - B gas constant - C heat capacity - C _p heat capacity at constant pressure - C _v heat capacity at constant volume - c ₀ acoustic velocity in the mixture - c _l acoustic velocity in the liquid - C _f flow resistance coefficient - G mass rate of flow - g gravitational acceleration - L latent heat of evaporation - l initial perturbation width - M Mach number - Nu Nusselt number - P pressure - Pr Prandtl number - R bubble radius - (3P ₀/R ₀ ² _f )^–1 bubble resonance frequency square - T temperature - U medium motion velocity - W heavy phase velocity - W light phase velocity - We Weber number - heat release coefficient - dispersion coefficient - void fraction - adiabatic index - film thickness - dimensionless film thickness - kinematic viscosity coefficient - dynamical viscosity coefficient - dissipation coefficient in the mixture - dispersion parameter - _f liquid phase density - light phase density - heat conductivity - surface tension - frequency, ₀ ² =3P ₀/ _f R ₀ ²     

Concentration dependence of the critical viscoelastic properties of gelatin at the gel point

Gelatin gel properties have been studied through the evolution of the storage [G()] and the loss [G()] moduli during gelation or melting near the gel point at several concentrations. The linear viscoelastic properties at the percolation threshold follow a power-law G()G() and correspond to the behavior described by a rheological constitutive equation known as the Gel Equation. The critical point is characterized by the relation: tan = G/G = cst = tan ( · /2) and it may be precisely located using the variations of tan versus the gelation or melting parameter (time or temperature) at several frequencies. The effect of concentration and of time-temperature gel history on its variations has been studied. On gelation, critical temperatures at each concentration were extrapolated to infinite gel times. On melting, critical temperatures were determined by heating step by step after a controlled period of aging. Phase diagrams [T = f(C)] were obtained for gelation and melting and the corresponding enthalpies were calculated using the Ferry-Eldridge relation. A detailed study of the variations of A with concentration and with gel history was carried out. The values of which were generally in the 0.60–0.72 range but could be as low as 0.20–0.30 in some experimental conditions, were compared with published and theoretical values.     

A third order scheme in the vlasov theory and some consequences in the evolution of few body systems

Summary A set of implemented evolution equations, describing the coherent nonlinear interaction of plasma waves, based on the perturbation method, has been derived, taking into account initial value effects and third order nonlinearities in the modal amplitudes.The equations reduce, in the appropriate limit, to well known stochastic triplets of hydrodynamic type.It is argued that, the stochastization mechanism of the decay instability in strongly damped regime, may be interpreted as a Duffing-type behavior.

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Sommario Si presenta un sistema di equazioni di evoluzione descrivente l'interazione coerente nonlineare di onde di plasma, tenendo conto di effetti di condizioni iniziali e nonlinearità del terzo ordine nelle ampiezze modali. Le equazioni si riducono, nel limite appropriato, a ben noti tripletti stocastici di tipo idrodinamico.Si ipotizza che il processo di stocastizzazione della instabilità di decadimento, in regime di forte dissipazione, possa essere interpretato da un modello dinamico del tipo Duffing.

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Lyst of greek symbols omega (lower case)=frequency - delta (1.c.)=partial derivative - pi (1.c.)=greek pi (=3,14r. units) in (26) - Sigma (Capital case)=Summation symbol - Delta (C.c)=def. as in (14) - epsilon (1.c.) def. as in (10) - sigma (1.c.)=def. as in (36) - gamma (1.c.)=def. as in (37) - beta (1.c.)=def. as in (37) - ro, (1.c.)=def. as in (37) - alfa (1.c.)=def. in connection with _k in (60) - Gamma (C.c.)=def. as in (63) and (66), (67) - delta (1.c.)=def. as in (66) - psi (1.c.)=def. as in (75) - fi (1.c.)=def. in (71) in connection with ₀ - Fi (C.c.)=def. as in (75) - Omega (C.c.)=def. in (78)     

Necessary and sufficient conditions for complete blow-up and extinction for one-dimensional quasilinear heat equations

We characterize the occurrence of complete or incomplete blow-up (and extinction) for a general quasilinear heat equation of the form in terms of the constitutive functions and f We assume that (u)>0 for u>0 and that f(u)0. For the positive sign + before f(u) in (HE), with f(u) superlinear as u, blow-up occurs in finite time: sup _x u(x, t) as tT<. For the negative sign, we consider the case of singular absorption: f(u) as u0. Then initially positive solutions vanish at some point in finite time (extinction), and a singularity in the equation occurs there. An important aspect of blow-up or extinction problems is the possibility of having a nontrivial extension of the solution for t>T, i.e., after the singularity occurs. If such continuation exists, we say that the blow-up (extinction) is incomplete; otherwise it is called complete. Our characterization is based on the qualitative behaviour of the family of travelling-wave solutions and a proper use of the Intersection-Comparison argument. The analysis applies to other nonlinear models, like the equations with gradient-dependent diffusivity.     

Thermal free convection from a solid sphere

Summary Thermal free convection from a sphere has been studied by melting solid benzene spheres in excess liquid benzene (Pr=8,3; 10⁸<Gr<10⁹). Overall heat transfer as well as local heat transfer were investigated. For the effect of cold liquid produced by the melting a correction has been applied. Results are compared with those obtained by other workers who used alternative experimental methods.Nomenclature coefficient of heat transfer - d characteristic length, here diameter of sphere - thermal conductivity - g acceleration of free fall - cubic expansion coefficient - T temperature difference between wall and fluid at infinity - kinematic viscosity - density - c specific heat capacity - a thermal diffusivity (=/c) - D diffusion coefficient - Nu dimensionless Nusselt number (=d/) - Nu* the analogous number for mass transfer (=kd/D) - mean value of Nusselt number - Gr dimensionless Grashof number (=gd ³T/ ²) - Gr* the analogous number for mass transfer (=gd ³x/ ²) - Pr dimensionless Prandtl number (=/a) - Sc dimensionless Schmidt number (=/D)     

Free convection on an arbitrarily inclined plate with uniform surface heat flux

This paper proposed a proper inclination parameter and transformation variables for the analysis of free convection from an inclined plate with uniform surface heat flux to fluids of any Prandtl number. Very accurate numerical results and a simple correlation equation are obtained for arbitrary inclination from the horizontal to the vertical and for 0.001 Pr. Maximum deviation between the correlated and calculated data is less than 1.2%.

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Freie Konvektion an einer beliebig geneigten Platte mit erheblicher Wärmestromdichte an der Oberfläche

Zusammenfassung Für die Berechnung von freier Konvektion von Fluiden mit beliebiger Prandtl-Zahl an einer geneigten Platte mit einheitlicher Wärmestromdichte an der Oberfläche werden ein zweckmäßiger Neigungsparameter und Transformationsvariablen eingeführt. Sehr genaue numerische Ergebnisse und eine einfache Korrelationsgleichung wurden für beliebige Neigungen zwischen der Horizontalen und der Vertikalen und für 0.001Pr erhalten. Die größte Abweichung zwischen Korrelations- und berechneten Daten liegt bei weniger als 1.2%.

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Nomenclature f reduced stream function - g gravitational acceleration - h local heat transfer coefficient - k thermal conductivity - Nu local Nusselt number - p static pressure difference - Pr Prandtl number - q _w wall heat flux - Ra* modified local Rayleigh number,g(q _w x/k)x ³/ - T fluid temperature - T temperature of ambient fluid - u velocity component inx-direction - v velocity component iny-direction - x coordinate parallel to the plate - y coordinate normal to the plate Greek symbols thermal diffusivity - thermal expansion coefficient - (Ra* |sin|)^1/5/( Ra* cos)^1/6 - ( Ra* cos)^1/6+( Ra*|sin|)^1/5 - (y/x) - dimensionless temperature, (T–T )/(q _w x/k) - kinematic viscosity - [1+( Ra* cos)^1/6/( Ra*|sin|)^1/5]^–1 - density of fluid - Pr/(1+Pr) - _w wall shear stress - angle of inclination measured from the horizontal - stream function - dimensionless static pressure difference, p x ²/ ⁴     

The boundary-layer flow past a suddenly heated vertical surface in a saturated porous medium

The boundary-layer flow generated on an impermeable vertical surface in a saturated porous medium is considered in the case when wall heating at a rate proportional tox is switched on at timet=0, (x measures distance along the wall and is a constant). The similarity equations which hold in the limit of larget are discussed and are shown to have a solution only for >–1. The behaviour of the solution as –1 and as is obtained. Numerical solutions of the initial value problem are then obtained for a range of values of . A direct numerical integration is possible for 1, while an iterative procedure is required for <1, with the numerical scheme becoming unstable for =–0.5.

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Grenzschichtströmung an einer plötzlich aufgeheizten vertikalen Fläche, in einem gesättigten porösen Medium

Zusammenfassung Es wird die an einer undurchlässigen, vertikalen Fläche hervorgerufene Grenzschichtströmung im Falle eines Einschalten der Heizung beit=0 betrachtet. Die Stärke der Wandheizung is proportional zux , wobeix die Koordinate längs der Wand ist und eine Konstante. Die Ähnlichkeitsgleichungen werden für den Bereich von großen Zeitent besprochen und es wird gezeigt, daß eine Lösung nur für >–1 vorliegt. Es wird das Verhalten der Lösungen für –1 und erhalten. Numerische Lösungen für die Anfangsbedingungen des Problems werden für eine Reihe von -Werten errechnet. Eine direkte numerische Integration ist für 1 möglich, während für <1 eine Iteration erforderlich ist, wobei das numerische Verhalten für =–0.5 instabil wird.

     

Theoretical derivation of tangential velocity profiles in a flat vortex chamber-influence of turbulence and wall friction

Summary As part of a study on the hydrodynamics of a cyclone separator, a theoretical investigation of the flow pattern in a flat box cyclone (vortex chamber) has been carried out. Expressions have been derived for the tangential velocity profile as influenced by internal friction (eddy viscosity) and wall friction. The most important parameter controlling the tangential velocity profile is = –u ₀ R/(v+ ), where u ₀ is the radial velocity at the outer radius R of the cyclone, the kinematic liquid viscosity and is the kinematic eddy viscosity. For values of greater than about 10 the tangential velocity profile is nearly hyperbolic, for smaller than 1 the tangential velocity even decreases towards the centre. It is shown how and also the wall friction coefficient may be obtained from experimental velocity profiles with the aid of suitable graphs. Because of the close relation between eddy viscosity and eddy diffusion, measurements of velocity profiles in flat box cyclones will also provide information on the eddy motion of particles in a cyclone, a motion reducing its separation efficiency.List of symbols A cross-sectional area of cyclone inlet - h height of cyclone - p static pressure in cyclone - p static pressure difference in cyclone between two points on different radius - r radius in cyclone - r ₁ radius of cyclone outlet - R radius of cyclone circumference - u radial velocity in cyclone - u ₀ radial velocity at circumference of flat box cyclone - v tangential velocity - v ₀ tangential velocity at circumference of flat box cyclone - w axial velocity - z axial co-ordinate in cyclone - friction coefficient in flat box cyclone (for definition see § 5) - ₁ value of friction coefficient for ₁<< ₂ - ₂ value of friction coefficient for ₂<<1 - = - ₁ value of for ₁<< ₂ - ₂ value of for ₂<<1 - thickness of laminar boundary layer - =/h - turbulent kinematic viscosity - ratio of z to h - k ratio of height of cyclone to radius R of cyclone - parameter describing velocity profile in cyclone =–u ₀ R/(+) - kinematic viscosity of fluid - density of fluid - ratio of r to R - ₁ value of at outlet of cyclone - ₂ value of at inner radius of cyclone inlet - _w shear stress at cyclone wall - angular momentum in cyclone/angular momentum in cyclone inlet - ₁ value of at = ₁ - ₂ value of at = ₂     

Flow in porous media II: The governing equations for immiscible,two-phase flow

The Stokes flow of two immiscible fluids through a rigid porous medium is analyzed using the method of volume averaging. The volume-averaged momentum equations, in terms of averaged quantities and spatial deviations, are identical in form to that obtained for single phase flow; however, the solution of the closure problem gives rise to additional terms not found in the traditional treatment of two-phase flow. Qualitative arguments suggest that the nontraditional terms may be important when / is of order one, and order of magnitude analysis indicates that they may be significant in terms of the motion of a fluid at very low volume fractions. The theory contains features that could give rise to hysteresis effects, but in the present form it is restricted to static contact line phenomena.Roman Letters (, = , , and ) A interfacial area of the- interface contained within the macroscopic system, m² - A _e area of entrances and exits for the -phase contained within the macroscopic system, m² - A interfacial area of the- interface contained within the averaging volume, m² - A ^* interfacial area of the- interface contained within a unit cell, m² - A _e ^* area of entrances and exits for the-phase contained within a unit cell, m² - g gravity vector, m²/s - H mean curvature of the- interface, m^–1 - H area average of the mean curvature, m^–1 - H – H , deviation of the mean curvature, m^–1 - I unit tensor - K Darcy's law permeability tensor, m² - K permeability tensor for the-phase, m² - K viscous drag tensor for the-phase equation of motion - K viscous drag tensor for the-phase equation of motion - L characteristic length scale for volume averaged quantities, m - characteristic length scale for the-phase, m - n unit normal vector pointing from the-phase toward the-phase (n = –n ) - p _c p – P , capillary pressure, N/m² - p pressure in the-phase, N/m² - p intrinsic phase average pressure for the-phase, N/m² - p – p , spatial deviation of the pressure in the-phase, N/m² - r ₀ radius of the averaging volume, m - t time, s - v velocity vector for the-phase, m/s - v phase average velocity vector for the-phase, m/s - v intrinsic phase average velocity vector for the-phase, m/s - v – v , spatial deviation of the velocity vector for the-phase, m/s - V averaging volume, m³ - V volume of the-phase contained within the averaging volume, m³ Greek Letters V /V, volume fraction of the-phase - mass density of the-phase, kg/m³ - viscosity of the-phase, Nt/m² - surface tension of the- interface, N/m - viscous stress tensor for the-phase, N/m² - / kinematic viscosity, m²/s