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Vol 53, No 2 (2018)

Article

Vortex Motion of an Incompressible Polymer Liquid in the Cylindrical Near-Axial Zone

Blokhin A.M., Semenko R.E.

Abstract

The time-dependent mathematical model describing the vortex motion of an incompressible polymeric liquid is discussed. In the steady-state case certain particular solutions are found. In the case of the steady-state pressure along the axis of cylinder, a version of deriving this model for both fixed and free boundaries is given.

Fluid Dynamics. 2018;53(2):177-188
pages 177-188 views

Steady Flows in an Oscillating Spheroidal Cavity with Elastic Wall

Kozlov V.G., Sabirov R.R., Subbotin S.V.

Abstract

The steady flow arising in a spheroidal cavity with periodically-deformed elastic wall is studied experimentally. It is found that average flows whose intensities and structures depend on the wall oscillation frequency and amplitude can develop in the fluid. The average flow is generated in the Stokes boundary layer whose relative thickness is characterized by the dimensionless frequency of the vibrational action. Flow in the form of a pair of toroidal vortices which occupy the entire cavity volume can be observed over the range of low dimensionless frequencies when the boundary layer thickness is comparable with the characteristic cavity dimension. Increase in the dimensionless frequency (decrease in the relative thickness of the Stokes layers) leads to a displacement of the primary vortices towards the cavity boundary. In this case secondary vortices with opposite swirling are formed in the central part of the cavity above the primary vortices. The further increase in the dimensionless frequency leads to development of the secondary vortices and growth of the flow intensity. The large-scale secondary vortices occupy almost the entire cavity volume over the range of high dimensionless frequencies. The dependences of the regimes of average flows and their intensities on the control dimensionless parameters, the oscillation amplitude and frequency, are found on the basis of the results of the investigation.

Fluid Dynamics. 2018;53(2):189-199
pages 189-199 views

Local Energy Dissipation Rate in an Agitated Vessel—a Comparison of Evaluation Methods

Šulc R., Ditl P.

Abstract

There are two main groups of local turbulent energy dissipation rate (ε) evaluation methods, namely (i) velocity gradient methods and (ii) fitting the energy spectrum function. We calibrated our measurements and then applied these methods to evaluate ε from our measurements. The experiments were carried out in the region below the impeller, wherewe assumed the existence of local isotropic turbulence, which is the main assumption for all ε evaluation methods. However, the results differed from each other. Predictions obtained by the methods dealt with here are compared on the basis of our experimental program, which also brings in data obtained on relatively large vessels 0.3 and 0.4 m in inner diameter and two liquid viscosities under fully developed turbulence (Re > 50 000).

Fluid Dynamics. 2018;53(2):200-211
pages 200-211 views

Vortex Shedding: A Review on Flat Plate

Teimourian A., Yazdi S.G., Hacisevki H.

Abstract

Flat plates, both single and in tandem or side by side arrangement, are widely used in many engineering applications. Despite vast investigations of the flow structures and wakes downstream of these bluff bodies, this unsteady phenomenon yet remains a fundamental issue in many industrial applications. This paper reviews the state of the art concerning the flow over flat plates in different arrangements focusing on plates normal to the flow. Turbulent wake regions are discussed for the flat plates in side by side or tandem arrangement. Numerical studies are reviewed with emphasis on the realized turbulent models. The effect of the chosen turbulence model on the prediction of the wake region is discussed.

Fluid Dynamics. 2018;53(2):212-221
pages 212-221 views

Steady Vortex Ring with Isochronous Flow in the Vortex Core

Akinshin R.V., Kopiev V.F., Chernyshev S.A., Yudin M.A.

Abstract

Steady-state solutions to the problem of a thin vortex ring in an inviscid incompressible fluid in infinite space are investigated. The Fraenkel procedure is used to construct the steady-state solutions. In this procedure a given vorticity distribution in plane flow with circular streamlines is transformed into a steady vortex ring using an expansion in the ring thinness parameter. For example, a two-dimensional vortex of constant vorticity is transformed into a steady vortex ring with the uniform distribution in which the absolute value of vorticity is proportional to the distance from the axis of symmetry. The principal aim of our study is to construct the algorithm of finding the flow for an isochronous vortex ring in which the periods of revolution are the same for all the liquid particles in the vortex core. The problem is that the two-dimensional distribution which goes over in the isochronous ring in accordance with the Fraenkel procedure is unknown in advance. In particular, the ring with the uniform distribution is not isochronous despite the isochronism of the initial two-dimensional flow. In this connection the Fraenkel procedure is significantly modified so that the initial two-dimensional vorticity distribution is determined in each of the steps of the iteration procedure. The solution for the vortex ring with the uniform distribution obtained in the present study is significantly used to construct the isochronous solution. The necessary corrections to the former solution are calculated in each step. Obtaining of the isochronous flow is the key step for the investigation of stability of three-dimensional oscillations of the vortex ring since the oscillation spectrum of this flow is discrete.

Fluid Dynamics. 2018;53(2):222-233
pages 222-233 views

Dipole Electromagnetic Radiation by a Charged Drop Oscillating in a Uniform Electrostatic Field

Grigor’ev A.I., Kolbneva N.Y., Shiryaeva S.O.

Abstract

The intensity of electromagnetic radiation generated by a charged drop oscillating in a uniform electrostatic field is studied within the framework of analytical calculations retaining the terms of the second order of smallness with respect to the ratio of the droplet oscillation amplitude to the droplet radius. It is found that the charge induced in the drop surface oscillations generates a dipole radiation detected in the first-order calculations and a self-charge detected with allowance for the second-order terms only. It is shown that the order of the magnitude of the total intensity of radiation generated by a cloud can be determined from small-droplet radiation. Among two radiation sources, namely, the radiation generated by small droplets oscillating at low modes and the radiation generated by hydrometeors oscillating at high modes, the first plays a dominant role.

Fluid Dynamics. 2018;53(2):234-247
pages 234-247 views

Acoustic Waves in a Liquid with Solid Particles and Gas Bubbles

Gubaidullin D.A., Fedorov Y.V.

Abstract

The mathematical model which determines acoustic wave propagation in a mixture of liquid with gas bubbles and solid particles is proposed. A system of differential equations is written and the dispersion relation is derived. Low- and high-frequency asymptotics of the phase velocity in the mixture considered are found and illustrated. The effect of solid particles and gas bubbles on acoustic wave dispersion and dissipation is indicated. For the mixture of fluid with solid particles considered the speed of sound is compared with available experimental data.

Fluid Dynamics. 2018;53(2):248-254
pages 248-254 views

Single-Fluid Model of a Mixture for Laminar Flows of Highly Concentrated Suspensions

Gavrilov A.A., Shebelev A.V.

Abstract

A model of laminar flow of a highly concentrated suspension is proposed. The model includes the equation of motion for the mixture as a whole and the transport equation for the particle concentration, taking into account a phase slip velocity. The suspension is treated as a Newtonian fluid with an effective viscosity depending on the local particle concentration. The pressure of the solid phase induced by particle-particle interactions and the hydrodynamic drag force with account of the hindering effect are described using empirical formulas. The partial-slip boundary condition for the mixture velocity on the wall models the formation of a slip layer near the wall. The model is validated against experimental data for rotational Couette flow, a plane-channel flow with neutrally buoyant particles, and a fully developed flow with heavy particles in a horizontal pipe. Based on the comparison with the experimental data, it is shown that the model predicts well the dependence of the pressure difference on the mixture velocity and satisfactorily describes the dependence of the delivered particle concentration on the flow velocity.

Fluid Dynamics. 2018;53(2):255-269
pages 255-269 views

Seepage Consolidation under Plane Deformation of Elastic Half-Space

Kosterin A.V., Skvortsov É.V.

Abstract

The process of seepage consolidation of elastic saturated half-space under the action of an arbitrary normal surface load is investigated in the case of plane deformation. The fluid and skeleton grains are assumed to be incompressible. A new mathematical model of consolidation is proposed with the use of the compatibility equation. Analytic dependences for the sum of effective normal stresses and fluid pressure are found on the basis of this model. The total normal stresses are explicitly expressed in terms of these dependences.

Fluid Dynamics. 2018;53(2):270-276
pages 270-276 views

Onset of Convection in a Cylindrical Container with a Free Boundary

Andreev V.K., Magdenko E.P.

Abstract

The problem of small perturbations of the equilibriumstate of a viscous, heat-conducting fluid in a cylindrical container with a deformable free upper boundary, on which heat exchange with the ambient medium is preassigned, is studied. The mathematical modeling of convection is based on Oberbeck–Boussinesq equations. The spectral problem thus obtained is solved using the tau method. As a result, the dependence of the imaginary part of the complex decrement on the Marangoni number is obtained. In the case of monotonic perturbations the neutral curves are plotted as functions of a geometrical parameter, namely, the cylinder height-to-radius ratio. The dependence of the Marangoni number on the physical parameters of the fluid is also obtained.

Fluid Dynamics. 2018;53(2):277-284
pages 277-284 views

Nonlinear Instability in the Region of Laminar-Turbulent Transition in Supersonic Three-Dimensional Flow over a Flat Plate

Lipatov I.I., Tugazakov R.Y.

Abstract

Direct numerical simulation is applied to obtain laminar-turbulent transition in supersonic flow over a flat plate. It is shown that, due to the nonlinear instability, Tollmien–Schlichting waves generated in the boundary layer lead to the formation of oblique disturbances in the flow. These represent a combination of compression and expansion waves, whose intensities can be two orders higher than that of external harmonic disturbances. The patterns of the three-dimensional flow over the plate are presented and the structures of the turbulent flat-plate boundary layers are described for the freestream Mach numbers M = 2 and 4.

Fluid Dynamics. 2018;53(2):285-295
pages 285-295 views

Optimal Axisymmetric Noses of Bodies in a Flow. Calculations and Experiments

Bol’shiyanov I.P., Zakharov N.N., P’yankov K.S., Tillyaeva N.I.

Abstract

The distinctive features of directmethods for contouring axisymmetric noses of bodies in a supersonic flow are discussed. The nose of a body of revolution in a supersonic flow, optimal with respect to the wave drag, includes a forward-looking flat face adjoining through a bend a sloping region of given aspect ratio (length-to-base-radius ratio), which, in turn, adjoins, again through a bend, the main part of the body. The above-mentioned sloping region can have, depending on its length, some additional internal bends. The presence of bends in a contoured configuration can often be undesirable, owing to strength, thermal, or others restrictions. For this reason, in solving the optimal contouring problems by means of direct methods analytical approximations of the unknown contour are often used, which leads to an increase in the drag of the optimized configuration. The degree of the increase in the drag of the nose part of a body of revolution in the cases of the local smoothing of bends in the optimal configuration and the global variation of its shape on the basis of an analytical approximation is investigated. It is shown that an increase in the drag of the nose part of a body of revolution owing its ineffective approximation can be many times greater than the gain due to optimization. The results of calculations are confirmed by the experimental data obtained.

Fluid Dynamics. 2018;53(2):296-304
pages 296-304 views

On the Reasonability of Taking the Volume Viscosity Coefficient into Account in Gas Dynamic Problems

Nikitchenko Y.A.

Abstract

The flow models are considered in the first (Navier–Stokes) approximation. The effect of the volume viscosity coefficient on the solutions obtained is investigated with reference to the problem of the plane shock wave profile. It is shown that taking the volume viscosity coefficient into account makes it possible to improve the solution for the flows with low dynamic nonequilibrium for which the first-approximation models are justified. It is preferable to use two-temperature flow models under the conditions of high dynamic nonequilibrium.

Fluid Dynamics. 2018;53(2):305-314
pages 305-314 views

Efficient Approach to Description of Heat Transfer and Multicomponent Diffusion in Ionized Gases

Kolesnikov A.F.

Abstract

The formulas for the heat fluxes of heavy components and electrons as well as the Stefan–Maxwell relations for the diffusion fluxes in amagnetic field are derived for amulticomponent two-temperature plasma with regard to the higher-order approximations in orthogonal expansions of the component distribution functions in Sonine polynomials. For the complex transport coefficients of heavy components and electrons exact formulas are obtained in the significantly simpler form as compared with the standard procedure of the Chapman–Enskog method with the minimum number of minimum-order matrix inversions.

Fluid Dynamics. 2018;53(2):315-324
pages 315-324 views

Three-Dimensional Problem of Radiative Gasdynamics of the Apollo-4 Command Module during Superorbital Atmospheric Entry

Surzhikov S.T.

Abstract

The three-dimensional problem of radiative gasdynamics of the superorbital entry of the Apollo-4 command module into the dense terrestrial atmosphere at an angle of attack of 25° is numerically solved. The flow conditions corresponding to the flight velocity V = 10.5 km/s at an altitude H = 67.3 km are considered in detail. The distributions of the densities of convective and radiative heat fluxes along the surface in a flow are obtained. The spectral composition of the thermal radiation attaining the surface is studied. The results of the calculations are successfully compared with the data of two-dimensional calculations.

Fluid Dynamics. 2018;53(2):325-336
pages 325-336 views