The effect of free stream turbulence on the momentum,heat and mass transfer during flow around a sphere

On the basis of our own experimental investigations of the effect of the fluid stream turbulence on the mean heat transfer, a possibility of significant (up to about 60 per cent) intensification of the process was shown. In the second part of this work, the authors attempted to analyze phenomena which result in heat layer. The significant role of three-dimensional disturbances of the Goertler type in the process of formation of “pseudo-laminar” boundary layer, was emphasized.     

Research on heat transfer of two-phase dispersed flow in narrow annular channel

Narrow channel heat transfer technique is a new developing heat transfer technique in recent years. As the temperature of droplet, steam and wall are decided by forced convection heat transfer between the steam and the wall, between the droplet and the wall, between the steam and the droplet and radiation heat transfer, which makes heat transfer mechanism of dispersed flow be difficultly interpretative. Dispersed flow in narrow annular channel is analyzed in the paper, investigating the influence of all kinds of heat transfer processes on dispersed flow, building annular channel dispersed flow model using thermodynamic non-equilibrium model. Calculation results show heat transfer is mainly controlled by heat transfer process between steam and wall. When temperature is low, radiation can be ignored on heat transfer coefficient calculation. The calculation of model can provide a reference for engineering application of steam generator, refrigeration system and so on.     

Effect of a liquid dispersed phase on the wall flow structure in static mixer

The effect of a liquid dispersed on the wall flow structure in static mixer is analyzed by using an electrochemical method. Both laminar and turbulent flows have been investigated. The axial wall velocity gradient and turbulent intensity have been studied along the static mixer in both flow regimes and for different dispersed phase concentrations. The spectral analysis of the wall velocity gradient fluctuations was analyzed in the turbulent regime. For volume fraction higher than 5%, the effect of the dispersed liquid phase is very important for all the studied parameters. The turbulence associated to the dispersed phase leads to an increase of the energy dissipation in the static mixer and also to a modification of energy dissipation mechanism.     

Multicomponent diffusion and heat exchange during the flow of an ionized gas in chemical equilibrium about a body

In the present paper, we investigate the flow of a multicomponent, partially ionized gas mixture in the boundary layer around an impermeable surface; the state in the boundary layer being one of chemical equilibrium. As an example, the flow of partially ionized air about a sphere is considered. The chemical composition at every point of the boundary layer with running values of the pressure, temperature, and concentrations of the chemical elements was found by Newton's method, parallel with the integration of the fundamental system of nonself-similar differential equations by the curve-fitting method. Also discussed is another method of finding the composition, which is more economical from the point of view of expenditure of machine time. It is found that the dimensionless heat flux to the wall at the front critical point of the sphere can be 26% larger for constant concentrations of the chemical elements than it is for variable concentrations.Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 3, pp. 53–59, May–June, 1972.The author thanks G. A. Tirskii for discussing the work.     

Convective heat exchange of a viscoplastic fluid with temperature-dependent rheological characteristics during structural flow in a circular pipe

Heat exchange in a viscoplastic liquid moving in a circular pipe is investigated, taking into account the dependence of plastic viscosity and ultimate shear stress on temperature. A system of motion, energy, and continuity equations transformed under the assumption that the Pe and Pr numbers are much greater than 1 is solved on a computer by the method of finite differences using iterations. Results of the numerical solutions for the exponential form of the dependences of the rheological characteristics on temperature are analyzed in detail. A comparison of the numerical solutions with well-known theoretical solutions in particular cases and also with experimental data indicates their high precision.     

Effect of fluid boundaries on flow around a low-aspect ratio wing

Large eddy simulation is applied to investigate flow around a finite-aspect-ratio wing in motion in a stratified fluid in different positions. It is shown that the wing position relative to a pycnocline has a considerable effect on the hydrodynamic wake development and the internal wave structure.     

Laminar heat exchange on sharp and blunt plates in a hypersonic air flow

The results of an experimental investigation and numerical simulation of heat exchange are given for sharp and blunt plates in a hypersonic air flow. The experiments were carried out in a Ludwig-type wind tunnel at hypersonic Mach numbers and a Reynolds number Re_L which varied over the range from 0.24 10⁶ to 1.31 10⁶. The bluntness radius r was varied over the range from 0.008 mm (almost sharp plate) to 4 mm (the corresponding Reynolds numbers Re_r from 15 to 4 10⁴). The numerical simulation was carried out by solving the complete two-dimensional Navier-Stokes equations. The experimental data were correlated using the well-known viscous hypersonic interaction parameters.__________Translated from Izvestiya Rossiiskoi Academii Nauk, Mekhanika Zhidkosti i Gaza, No. 1, 2005, pp. 168–180. Original Russian Text Copyright © 2005 by Borovoi, Egorov, Skuratov and Struminskaya.     

Effect of the domain spanwise periodic length on the flow around a circular cylinder

We assess the effect of the choice of spanwise periodic length on simulations of the flow around a fixed circular cylinder. The Reynolds number is set to 400 because, at this value, both lift coefficient and shedding frequency show significant drop due to three-dimensional flow structures. From the analysis of the three-dimensionalities of the wake and of the integral quantities such as Strouhal number, RMS of lift coefficient and energy contained in the three-dimensional portion of the flow we obtain an estimate of the minimum spanwise length to satisfactorily represent the flow. Furthermore, we observe a distinct wake behavior when the spanwise length is approximately the mode B instability wavelength.     

Effect of magnetic field on 3D flow and heat transfer during solidification from a melt

We present the effect of a magnetic field on three-dimensional fluid flow and heat transfer during solidification from a melt in a cubic enclosure. The walls of the enclosure are considered perfectly electrically conducting and the magnetic field is applied separately in three directions. The finite-volume method with enthalpy formulation is used to solve the mathematical model in the solid and liquid phases. The results obtained by our computer code are compared with the numerical and experimental data found in the literature. For Gr = 5 × 10⁵ and Ha = 0, 25, 50, 75, and 100 (where Gr and Ha are the Grashof and Hartmann numbers, respectively), the effects of magnetic field on flow and thermal fields, and on solid/liquid interface shape are presented and discussed. The interface is localized with and without magnetic field. The results show a strong dependence between the interface shape and the intensity and orientation of magnetic field. When the magnetic field is applied along the X-direction, the magnetic stability diagrams (V_max–Ha) and (Nu_avg–Ha) show the strongest stabilization of the flow field and heat transfer.     

Radiative and convective heat transfer in hypersonic flow around a blunt body

The heat transfer in the vicinity of the critical point is investigated for hypersonic air flow around a blunt body. The gas-dynamical conservation equations are solved simultaneously with the radiative transport equation in integral form. Allowance is made for the viscosity, heat conduction, and the actual radiation parameters of air, including spectral line emission. Profiles are obtained for the thermodynamic variables along the critical line. The dependence of the radiative and convective components of the aerodynamic heating on the velocity and pressure ahead of the shock front as well as the radius of curvature of the blunt nose section is discussed. Approximate relations having the form of similarity laws are derived for the heat fluxes in the vicinity of the critical point. The limits of applicability of the thermodynamic equilibrium approximation in the shock-compressed layer are discussed. The influence of absorption of radiation from the compressed layer by the cold freestream on the aerodynamic heating is considered. Attention is given in this case to the dependence of the spectral absorption coefficient for the cold air on the intensity of the radiation incident upon it.Moscow. Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 5, pp. 112–123, September–October, 1972.