Theory of nonequilibrium effects associated with the flow of nonuniform fluids in porous media

It is of interest to study nonequilibrium effects associated with the motion of nonuniform fluids in a porous medium because they may have a considerable significance both for an understanding of the physics of flow in porous medium as well as for applications, primarily in the exploitation of oil and gas deposits. The aim of the present paper is to make a theoretical analysis of some aspects of the nonequilibrium state associated with the length of the process of establishment of capillary equilibrium, and also to consider possible consequences of these aspects.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 52–57, May–June, 1980.     

Nonlinear electromagnetic phenomena in a liquid with nonequilibrium electrical conductivity in an alternating magnetic field

On the basis of [1] this note examines nonlinear electromagnetic phenomena in a dense plasma brought about by the variation in its electrical conductivity as the electrical field changes. It is well known that the electrical conductivity depends on the electric field strength due to the following causes. The electrons in moving in the electric field receive energy from the field which may be considerable over the free path length. However it is difficult for this energy to be transferred to the heavy particles. In monatomic gases the energy exchange between electrons and heavy particles comes about basically as a result of elastic collisions. Thus a noticeable difference in electron and ion temperature, determined by the electron energy balance taking radiation losses into account, turns out to be possible even for relatively weak electric fields. In molecular gases, on the other hand, the fundamental energy exchange mechanism is the excitation of the rotational and oscillatory degrees of freedom of the molecules. Thus the electron energy in these gases is dissipated relatively easily, and the electron temperature is not observed to be noticeably higher than the atomic temperature. The concept of the characteristic “plasma field” E_p is introduced in [2], which is determined for an Isotropic plasma by the relation

$$E_R = \sqrt {3kTme^{ - 2\delta } (\omega ^2 + v_0 ^2 )} .$$     

Influence of flow field scaling on flashback of swirl flames

In this paper, the effect of geometrical scaling on the onset of flashback into a cylindrical premixing zone of a swirl flame is investigated. We discriminate two types of flashback. In the first type of flashback the flame propagates upstream inside an already present axial recirculation zone. This flashback is caused by turbulent burning along the vortex axis (TBVA¹) and is controlled by flame extinction inside the recirculation zone. The second type of flashback is caused by combustion induced vortex breakdown (CIVB²). This type of flashback is characterised by the aerodynamic influence of the combustion heat release that leads to propagation of the axial recirculation zone and the flame in upstream direction.To study the effects of geometrical scaling on the flow fields and the two types of flashback, the operation of two geometrically scaled burners are compared at equal Reynolds number. By this method it is possible to observe the flashback phenomena in similar swirl flow fields but with different turbulent scales affecting the combustion process. To check flow field similarity and to indentify the flashback type, the non-reacting and reacting flow fields have been examined by planar particle imaging velocimetry and simultaneous recording of the flame luminescence.It is shown that geometrical scaling of the burner shifts the equivalence ratio at which flashback occurs and that this shift is different for the two types of flashback. Consistency and inconsistency with known scaling and stability criterions is discussed. Analysing the fluid dynamics and turbulent combustion gives a first explanation of why CIVB and TBVA are affected differently by geometrical scaling at constant Reynolds number which is in good agreement with the experimental observations.     

Three-dimensional chemically nonequilibrium viscous shock layer on a catalytic surface with allowance for associated heat transfer

A three-dimensional flow of dissociating air past blunt bodies is investigated in the framework of the thin viscous shock layer theory. Multicomponent diffusion and homogeneous chemical reactions, including dissociation, recombination, and exchange reactions, are taken into account. The generalized Rankine-Kugoniot conditions are specified on the shock wave and the conditions which take into account the heterogeneous catalytic reactions, on the surface of the body. The viscous shock layer equations are solved together with the heat equations inside the coating, which is carbon with a deposited thin film of SiO₂, or quartz. The case of a thermally insulated surface is also considered. The problem for the case of the motion of a body along the re-entry trajectory into Earth's atmosphere is investigated numerically. The temperature of the surface and the heat flux toward it are given as a dependence on the height (tine) of the flight for different cases of the specification of the catalytic reactions. It is shown that the difference between the heat fluxes towards the thermally insulated surface and the fluxes toward the heat-conducting surface in the neighborhood of the stagnation point is of the order of 6–12% for all the cases considered. This makes it possible to decouple the solution of the problem of heat conduction in the body.Translated fron Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 140–146, November–December, 1985.deceased     

Stability of low-voltage arc with nonequilibrium ionization

A stability criterion is obtained for a low-voltage arc in the absence of ionization equilibrium. It is shown that the stability depends on the properties of the generation function. The example of a cesium arc of a thermionic converter illustrates the influence of a change of the electron temperature on the stability of a plasma.     

Effects of nonequilibrium of the plasma of a vapor aureole in an intense radiation field

Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 2, pp. 3–7, March–April, 1991.     

Strain field associated with brittle-fracture propagation in wide steel plates

The results of an experimental investigation concerned with the study of the strain field surrounding a brittle fracture propagating across a wide steel plate are presented in this paper. The data were obtained from tests of 6-ft wide steel plates that were instrumentated to measure surface strain and crack speed. The plates were tested at an average net applied stress of 19,000 psi, a temperature of about ?5° F, and with the notch-wedgeimpact method for fracture initiation. Several plates were tested under similar conditions and the results were superimposed to give a representative picture of the strain distribution on the surface of a plate in the region of the tip of a propagating fracture. Contours of the maximum principal strain for various lengths of crack are presented. The studies indicate that for this particular specimen geometry and associated test conditions, the strain field surrounding the tip of the advancing fracture remains essentially unchanged after traversing about one-third of the width of a 6-ft wide plate.     

A nonequilibrium viscous shock-wave layer in the vicinity of the critical point with the associated heat exchange taken into account

Results are presented in this article of numerical calculations of a viscous shock layer with the associated heat exchange in the vicinity of the critical point of a spherical blunt body taken into account in the presence of nonequilibrium chemical processes in the shock layer and on the surface of the body about which the flow takes place. A number of papers [1–4], in which specification of the surface temperature of the obstacle was utilized, have been devoted to the numerical investigation of a nonequilibrium viscous shock layer. At the same time the surface temperature of a body varies in actual flight due to heating, and together with this there is catalytic activity of the material, which appreciably complicates the problem and necessitates the simultaneous treatment of the course of processes in the gaseous and solid phases. The use of a separate formulation is difficult in this case, since the formulas for the thermal flux from the gaseous phase are of an estimative nature [5] when a volume nonequilibrium chemical reaction is present for a surface having an arbitrary catalytic activity. Taking account of the associated heat exchange has been done before for a number of problems of boundary-layer theory [6, 7], and in this case it has permitted determining the characteristics which are most important from the practical standpoint under conditions of flight along a specified trajectory, as well as under specified time-independent conditions of flight at altitudes at which the approximation of a viscous shock layer is valid. The effect of catalytic activity is discussed for a number of surface materials, and it is shown that the use of the formulas of boundary layer theory can appreciably distort the behavior of the surface temperature as a function of time for a certain altitude range.Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 3, pp. 108–114, May–June, 1979.     

On two-dimensional laminar flows of a particulate suspension in the presence of gravity field

Three simple two-dimensional streaming motions of a mixture of solid particles with a continuous carrier fluid, or gas, in the presence of the gravity field are considered. These include flow of a mixture over an infinite stationary rigid plane perpendicular to the direction of the gravity field, flow near an oscillating rigid plane and flow in a mixture induced by a suddenly accelerated plane. The nature of the boundary conditions at the interface between a layer of sediment settling on the rigid boundary and the mixture above it suggests an introduction of the independent variables that enable simple analytical expressions for the solutions of the first two flows and a numerical solution by means of a Laplace transform in the last case.     

Two-dimensional mixed flows of a supersaturated and two-phase medium with nonequilibrium phase transitions

The singularities of two-dimensional interchannel flows of a condensing and damp vapor with nonequilibrium phase transitions which contain gas-dynamic discontinuities are investigated. A through-computation difference method is constructed for such flows. The results of the numerical investigation of steam flows with spontaneous condensation in supersonic plane nozzles containing a break in the walls and flow around a wedge are represented. It is shown that nonequilibrium condensation can result in a qualitative rearrangement of the wave structure of the flow which is impossible to obtain within the framework of the one-dimensional approach.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 87–93, July–August, 1978.     

A study on the flow field and local heat transfer performance due to geometric scaling of centrifugal fans

Scaled versions of fan designs are often chosen to address thermal management issues in space constrained applications. Using velocity field and local heat transfer measurement techniques, the thermal performance characteristics of a range of geometrically scaled centrifugal fan designs have been investigated. Complex fluid flow structures and surface heat transfer trends due to centrifugal fans were found to be common over a wide range of fan aspect ratios (blade height to fan diameter). The limiting aspect ratio for heat transfer enhancement was 0.3, as larger aspect ratios were shown to result in a reduction in overall thermal performance. Over the range of fans examined, the low profile centrifugal designs produced significant enhancement in thermal performance when compared to that predicted using classical laminar flow theory. The limiting non-dimensional distance from the fan, where this enhancement is no longer apparent, has also been determined. Using the fundamental information inferred from local velocity field and heat transfer measurements, selection criteria can be determined for both low and high power practical applications where space restrictions exist.     

Airflow behind strong shock front with account for nonequilibrium ionization and radiation

We consider the gas state behind a shock wave front in air with a velocity v10 km/sec. Nonequilibrium ionization and radiative transport are taken into account. We take into consideration the real air spectrum — the numerous lines, bands, and continuua. Account for the radiation leads to an integrodifferential system of equations for which a solution method is developed. As a result we obtain the gas parameter profiles behind the shock wave, which are affected by the relaxation processes and radiative cooling. The calculations were made for v=10–16 km/sec and a pressure p=10^–5–10^–2 atm ahead of the front.In order to obtain realistic results, we consider only the gas layer bounded by the shock and a surface parallel to it. It is assumed that the gas bounded by these planes is not irradiated from without. In this formulation still another defining parameter appears—the distancel between the planes. The calculations were made forl=1–100 cm.     

Steady temperature field associated with the flow of gassy oil in a porous medium

The steady thermal field associated with the flow of gassy oil through a porous medium is investigated with allowance for the Joule-Thomson and degassing effects. A formula is obtained for estimating the temperature anomalies at the well bottom on oil inflow intervals which correspond to a bottom pressure lower than the saturation pressure. Ufa. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No.1, pp. 113–116, January–February, 1994.     

Determining parameters in nonequilibrium flow of a gas with homogeneous condensation

Analytic expressions are obtained for the parameters which determine the number of particles (clusters) and their mean radius and the supercooling at the starting point of active homogeneous condensation (the Wilson point). With a given law p=f(T), such parameters are the temperature T_s at the dew point and the mean cooling rate = dT/dt of the gas from the dew point to the Wilson point. In this context, with T_s = const and = const, the processes of nonequilibrium homogeneous condensation in the P-T diagram corresponding to the various initial states after the Wilson point may be described approximately by a single curve. So the parameters T_s and are determining parameters for the whole process of nonequilibrium homogeneous condensation. Equations are given which enable us to estimate approximately the cooling rate for flows in nozzles and jets. Computation results are given for steady flow in a Laval nozzle and unsteady spherically symmetric expansion of a gaseous sphere into a vacuum; these results demonstrate the noted regularities. Despite the great amount of literature, both periodical and monograph, on the nonequilibrium condensation of vapors, the important question of the determining parameters for the process of a homogeneous nonequilibrium condensation has not been studied to any great extent [1].Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 80–87, May–June, 1985.     

Heat transfer associated with viscous two-dimensional channel flow in a transverse acoustic field

An analytic solution is proposed for the problem of the effect of a transverse resonant acoustic field on the heat transfer process in laminar two-dimensional channel flow.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 41–49, May–June, 1985.The author wishes to thank V. E. Nakoryakov for formulating the problem and discussing the results.