Role of the Knudsen layer in the problem of droplet evaporation

A study is made of the part played by the Knudsen layer in the problem of weak unsteady evaporation of a spherical droplet in its own vapor. It is shown that use of the classical Hertz—Knudsen formula may lead to appreciable errors, in particular, in the determination of the time required by the droplet temperature to relax to the state corresponding to steady evaporation.Translated from Izvestiya Akademii Nauk SSSR; Mekhanika Zhidkosti i Gaza, No. 1, pp. 127–131, January–February, 1984.     

Secondary flows in a layer with a free surface

The loss of stability of a plane-parallel incompressible viscous heat-conducting fluid flow in a horizontal layer subject to a longitudinal temperature gradient is considered. The lower surface of the layer is assumed to be rigid, while the upper one is free with a surface tension coefficient depending linearly on temperature. Both boundaries are assumed to be thermally-insulated. The critical value of the temperature gradient as a function of other relevant parameters is determined by analyzing the spectrum of the linearized problem. Secondary flows arising after the onset of instability are determined from an analysis of the full nonlinear problem using the expansion of the solution in a power series in terms of a supercritical state parameter in the vicinity of the bifurcation point. Three types of secondary flows are studied: plane two-dimensional waves propagating along the temperature gradient; plane waves travelling at a certain angle to the gradient; and three-dimensional waves propagating along the gradient. A numerical method of problem solution, based on the polynomial approximation, is described.Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 5, pp. 85–98, September–October, 1994.     

Supersonic dusty-gas flows with Knudsen effect in interphase momentum exchange

On the basis of the two-continuum model of dilute gas-solid suspensions, the dynamic behavior of inertial particles in supersonic dusty-gas flows past a blunt body is studied for moderate Reynolds numbers, when the Knudsen effect in the interphase momentum exchange is significant. The limits of the inertial particle deposition regime in the space of governing parameters are found numerically under the assumption of the slip and free-molecule flow regimes around particles. As a model problem, the flow structure is obtained for a supersonic dusty-gas point-source flow colliding with a hypersonic flow of pure gas. The calculations performed using the full Lagrangian approach for the near-symmetry-axis region and the free-molecular flow regime around the particles reveal a multi-layer structure of the dispersed-phase density with a sharp accumulation of the particles in some thin regions between the bow and termination shock waves. The project supported by the National Natural Science Foundation of China (90205024), and the Russian Foundation for Basic Research (RFBR grant No. 02-01-00770 and joint RFBR-NSFC grant No. 03-01-39004)     

A Knudsen layer in a flow with two-temperature relaxation

The boundary conditions are considered for the hydrodynamic equation of [1, 2] for highly nonequilibrium diatomic gas with vibrational relaxation.Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 6, pp. 38–43, November–December, 1972.     

Boundary conditions for flows with chemical reactions occurring on a surface

With the use of a solution of a model Boltzmann equation for a binary mixture in the Knudsen layer, we obtain the boundary conditions for the equations of gas dynamics when the reactionl _iA_il _jA_j (l _i molecules of A_i change intol _j molecules of A_j, and vice versa) is occurring on a surface. The boundary condition that we obtain differs from those that are usually applicable by the presence of terms of the same order. This confirms the conclusion arrived at by the authors in [1], where it was shown that if the Knudsen layer is left out of account, which is precisely what is usually done, it is impossible to obtain correct boundary conditions.Moscow. Translated from Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 129–138, January–February, 1972.     

Integral boundary layer relations in the theory of wave flows for capillary liquid films

A generalized method of deriving the model equations is considered for wave flow regimes in falling liquid films. The viscous liquid equations are used on the basis of integral boundary layer relations with weight functions. A family of systems of evolution differential equations is proposed. The integer parameter n of these systems specifies the number of a weight function. The case n = 0 corresponds to the classical IBL (Integral Boundary Layer) model. The case n ≥ 1 corresponds to its modifications called the WIBL (Weighted Integral Boundary Layer) models. The numerical results obtained in the linear and nonlinear approximations for n = 0, 1, 2 are discussed. The numerical solutions to the original hydrodynamic differential equations are compared with experimental data. This comparison leads us to the following conclusions: as a rule, the most accurate solutions are obtained for n = 0 in the case of film flows on vertical and inclined solid surfaces and the accuracy of solutions decreases with increasing n. Hence, the classical IBL model has an advantage over the WIBL models.     

Construction of solutions of the Boltzmann kinetic equation in a Knudsen layer

We consider the moment equation method for solving the Boltzmann equation in a Knudsen layer; the calculation of one of the moments of the collision integral is presented.     

Mixing in horizontally heterogeneous flows

An experimental study of mixing across density interfaces produced by laterally heterogenous turbulence is presented in this paper. The turbulence is generated by a flow or air bubles rising through a density interface produced by brine and fresh water. The mixing efficiency, , of the process is measured comparing the increase in potential energy with the available kinetic energy. We find that there is a decrease in the global mixing efficiency of the process with the length of the tank, the shape of (Ri) depends also on the air flow producing the turbulence, showing a geometrical limit to the ammount of kinetic energy which may be used for mixing.     

Confined viscoplastic flows with heterogeneous wall slip

The steady, pressure-driven flow of a Herschel-Bulkley fluid in a microchannel is considered, assuming that different power-law slip equations apply at the two walls due to slip heterogeneities, allowing the velocity profile to be asymmetric. Three different flow regimes are observed as the pressure gradient is increased. Below a first critical pressure gradient G ₁, the fluid moves unyielded with a uniform velocity, and thus, the two slip velocities are equal. In an intermediate regime between G ₁ and a second critical pressure gradient G ₂, the fluid yields in a zone near the weak-slip wall and flows with uniform velocity near the stronger-slip wall. Beyond this regime, the fluid yields near both walls and the velocity are uniform only in the central unyielded core. It is demonstrated that the central unyielded region tends towards the midplane only if the power-law exponent is less than unity; otherwise, this region rends towards the weak-slip wall and asymmetry is enhanced. The extension of the different flow regimes depends on the channel gap; in particular, the intermediate asymmetric flow regime dominates when the gap becomes smaller than a characteristic length which incorporates the wall slip coefficients and the fluid properties. The theoretical results compare well with available experimental data on soft glassy suspensions. These results open new routes in manipulating the flow of viscoplastic materials in applications where the flow behavior depends not only on the bulk rheology of the material but also on the wall properties.     

Exit plane and suction surface flows in an annular turbine cascade with a skewed inlet boundary layer

The flow in the exit plane and on the suction surface of an annular turbine cascade was examined experimentally for conditions of inlet boundary layer skewing similar to that found in a real turbine and for the collateral inlet as found in most cascade tests. Skewing was introduced by rotating the nose cone ahead of the cascade.At the cascade exit, the loss distribution pattern, as measured by a 3 hole cobra probe, showed that the corner vortex at the hub is displaced radially to almost a mid-span position by the skewed inlet boundary layer. This movement was attributed to the stronger endwall crossflows being radially directed as they strike and rise up onto the suction surface. The radial displacement and endwall crossflow effect was also seen in surface flow visualization studies.The overall cascade loss coefficient and deviation angle are significantly reduced by skewing. Traverses taken on the suction surface confirmed the separated flow effects seen in the flow visualization pictures.The general conclusion is that skewing plays a significant role in determining the flow phenomena in turbine cascades and that these effects should be borne in mind when interpreting the results taken from plane cascades.     

Kinetic theory of recondensation in a binary gas mixture with arbitrary Knudsen numbers

A rigorous solution of the problem of recondensation between two surfaces with arbitrary Knudsen numbers is possible only on the basis of a consecutive kinetic consideration. For the single-component case, this problem was solved in [1] using the BGK model of the collision integral in the kinetic equation. In [2], for the same purpose, the method of moments for Maxwellian molecules was used. The case of a binary mixture, in which one of the components is a noncondensing gas was discussed in [3, 4]. Under these circumstances, in [3], a single-relaxation lumped model was used for each component; the model did not reflect many of the properties of the exact collision integral. A more rigorous model (the collision integral in the Hamel form) was applied in [4]. Here there was written a system of integral equations for the hydrodynamic quantities, and its numerical solution is examined in several specific partial cases. In the present article, the problem of recondensation in a binary mixture is treated by the method of moments for Maxwellian molecules. For the case of small relative difference in the temperature of the surfaces, analytical expressions are obtained for the rates of mass transfer and the heat fluxes, making it possible to shed light on the principal special characteristics of the process of recondensation in a binary mixture.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 150–155, July–August, 1975.The authors thank R. Ya. Kucherov for his useful observations.     

Effect of thermodiffusion on intensity of surface burn-out in a heterogeneous turbulent boundary layer

On the basis of an analysis of the binary diffusion equation in the viscous sublayer of the turbulent boundary layer an estimate is given of the effect of thermodiffusion on the concentration of components at an impervious wall, on the permeability of the wall, and on the intensity of heating of the reactive surface. Experimental results are presented on the burnout of a graphite wall in mixtures of air with nitrogen, argon, and helium.Translated from Zhurnal Prikaldnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 5, pp. 119–125, September–October, 1972.     

On the surface equations in two-phase flows and reacting single-phase flows

This paper summarizes the mathematical surface equations which are useful in two-phase flows and single-phase reacting flows. The connection between the interfacial area concentration transport equation for two-phase flows and the flame surface density transport equation for turbulent reacting flows is established. Several analytical examples are given to clarify the physical significance of the different quantities involved in the different transport equations. An introduction to the mathematical treatment of anisotropic interfaces is also given. This theory is illustrated on two different numerical examples: a single inclusion in a simple shear and a single inclusion in an uni-axial elongation.