Nonlinear Magneto-Heat Transfer in a Fluid-Particle Suspension Flowing in a Non-Darcian Channel with Heat Source and Buoyancy Effects: Numerical Study
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A Two-Layer Turbulence Model for Simulating Indoor Airflow Part I
Energy and Buildings 33 +2001) 613±625 A two-layer turbulence model for simulating indoor air¯ow Part I. Model development Weiran Xu, Qingyan Chen* Department of Architecture, Massachusetts Institute of Technology, 77 Massachusetts Avenue, MA 02139, USA Received 2 August 2000; accepted 7 October 2000 Abstract Energy ef®cient buildings should provide a thermally comfortable and healthy indoor environment. Most indoor air¯ows involve combined forced and natural convection +mixed convection). In order to simulate the ¯ows accurately and ef®ciently, this paper proposes a two-layer turbulence model for predicting forced, natural and mixed convection. The model combines a near-wall one-equation model [J. Fluid Eng. 115 +1993) 196] and a near-wall natural convection model [Int. J. Heat Mass Transfer 41 +1998) 3161] with the aid of direct numerical simulation +DNS) data [Int. J. Heat Fluid Flow 18 +1997) 88]. # 2001 Published by Elsevier Science B.V. Keywords: Two-layer turbulence model; Low-Reynolds-number +LRN); k±e Model +KEM) 1. Introduction This paper presents a new two-layer turbulence model that performs two tasks: 1.1. Objectives 1. It can accurately predict flows under various conditions, i.e. from purely forced to purely natural convection. This Energy ef®cient buildings should provide a thermally model allows building ventilation designers to use one comfortable and healthy indoor environment. The comfort single model to calculate flows instead of selecting and health parameters in indoor environment include the different turbulence models empirically from many distributions of velocity, air temperature, relative humidity, available models. and contaminant concentrations. These parameters can be 2. -
Experimental Study of the Fluid Drag on a Torus at Low Reynolds Number. Dharmaratne Amarakoon Louisiana State University and Agricultural & Mechanical College
Louisiana State University LSU Digital Commons LSU Historical Dissertations and Theses Graduate School 1982 Experimental Study of the Fluid Drag on a Torus at Low Reynolds Number. Dharmaratne Amarakoon Louisiana State University and Agricultural & Mechanical College Follow this and additional works at: https://digitalcommons.lsu.edu/gradschool_disstheses Recommended Citation Amarakoon, Dharmaratne, "Experimental Study of the Fluid Drag on a Torus at Low Reynolds Number." (1982). LSU Historical Dissertations and Theses. 3743. https://digitalcommons.lsu.edu/gradschool_disstheses/3743 This Dissertation is brought to you for free and open access by the Graduate School at LSU Digital Commons. It has been accepted for inclusion in LSU Historical Dissertations and Theses by an authorized administrator of LSU Digital Commons. For more information, please contact [email protected]. INFORMATION TO USERS This reproduction was made from a copy of a document sent to us for microfilming. While the most advanced technology has been used to photograph and reproduce this document, the quality o f the reproduction is heavily dependent upon the quality of the material submitted. The following explanation of techniques is provided to help clarify markings or notations which may appear on this reproduction. t.The sign or “target” for pages apparently lacking from the document photographed is "Missing Page(s)” . If it was possible to obtain the missing page(s) or section, they are spliced into the film along with adjacent pages. This may have necessitated cutting through an image and duplicating adjacent pages to assure complete continuity. 2. When an image on the film is obliterated with a round black mark, it is an indication of either blurred copy because of movement during exposure, duplicate copy, or copyrighted materials that should not have been filmed. -
Sedimentation of Finite-Size Spheres in Quiescent and Turbulent Environments
Under consideration for publication in J. Fluid Mech. 1 Sedimentation of finite-size spheres in quiescent and turbulent environments Walter Fornari1y, Francesco Picano2 and Luca Brandt1 1Linn´eFlow Centre and Swedish e-Science Research Centre (SeRC), KTH Mechanics, SE-10044 Stockholm, Sweden 2Department of Industrial Engineering, University of Padova, Via Venezia 1, 35131 Padua, Italy (Received ?; revised ?; accepted ?. - To be entered by editorial office) Sedimentation of a dispersed solid phase is widely encountered in applications and envi- ronmental flows, yet little is known about the behavior of finite-size particles in homo- geneous isotropic turbulence. To fill this gap, we perform Direct Numerical Simulations of sedimentation in quiescent and turbulent environments using an Immersed Boundary Method to account for the dispersed rigid spherical particles. The solid volume fractions considered are φ = 0:5 − 1%, while the solid to fluid density ratio ρp/ρf = 1:02. The par- ticle radius is chosen to be approximately 6 Komlogorov lengthscales. The results show that the mean settling velocity is lower in an already turbulent flow than in a quiescent fluid. The reduction with respect to a single particle in quiescent fluid is about 12% and 14% for the two volume fractions investigated. The probability density function of the particle velocity is almost Gaussian in a turbulent flow, whereas it displays large positive tails in quiescent fluid. These tails are associated to the intermittent fast sedimentation of particle pairs in drafting-kissing-tumbling motions. The particle lateral dispersion is higher in a turbulent flow, whereas the vertical one is, surprisingly, of comparable mag- nitude as a consequence of the highly intermittent behavior observed in the quiescent fluid. -
Forces on Particles and Bubbles
Title Forces on Particles and Bubbles M. Sommerfeld Mechanische Verfahrenstechnik Zentrum für Ingenieurwissenschaften Martin-Luther-Universität Halle-Wittenberg D-06099 Halle (Saale), Germany www-mvt.iw.uni-halle.de Martin-Luther-Universität Halle-Wittenberg Content of the Lecture BBO equation and particle tracking Forces acting on particles moving in fluids Drag force Pressure, virtual mass and Basset Transverse lift forces Electrostatic force Thermophoretic and Brownian force Importance of the different forces Particle response time and Stokes number Behaviour of bubbles and forces Particle response to oscillatory flow filed Martin-Luther-Universität Halle-Wittenberg Equation of Motion 1 The equation of motion for particles in a quiescent fluid was first derived by Basset (1888), Bousinesque (1885), and Oseen (1927) BBO-equation. A rigorous derivation of the equation of motion for non-uniform Stokes flow was performed by Maxey and Riley (1983). The BBO-equation without the Faxen terms (due to curvature of the velocity field) is given by: d u 18 µ m Du d u P = F − − P − ∇ + ∇τ + F − P mP 2 mP (uF uP ) ( p ) 0.5 mF d t ρP DP ρP Dt d t Importance of d uF d uP the different t * − * ρ µ m d t d t * (u − u ) forces ??? + 9 F F P dt + F P 0 + m g ∫ * 1 2 P π ρP DP 0 (t − t ) t Accounts for d Derivative along D Substantial : : initial condition dt particle path Dt derivative 1: drag force 2: pressure term 3: added mass 4: Basset force (with initial condition) 5: gravity force Martin-Luther-Universität Halle-Wittenberg Equation of Motion 2 The calculation of particle trajectories requires the solution of several partial differential equations: particle location particle velocity particle angular velocity d x p d u d ω = u p p = p mp = ∑ Fi Ip T dt dt dt The consideration of heat and mass transfer requires the solution of two additional partial differential equations for droplet diameter and droplet temperature. -
(English Edition) a Review on the Flow Instability of Nanofluids
Appl. Math. Mech. -Engl. Ed., 40(9), 1227–1238 (2019) Applied Mathematics and Mechanics (English Edition) https://doi.org/10.1007/s10483-019-2521-9 A review on the flow instability of nanofluids∗ Jianzhong LIN†, Hailin YANG Department of Mechanics, State Key Laboratory of Fluid Power and Mechatronic Systems, Zhejiang University, Hangzhou 310027, China (Received Mar. 22, 2019 / Revised May 6, 2019) Abstract Nanofluid flow occurs in extensive applications, and hence has received widespread attention. The transition of nanofluids from laminar to turbulent flow is an important issue because of the differences in pressure drop and heat transfer between laminar and turbulent flow. Nanofluids will become unstable when they depart from the thermal equilibrium or dynamic equilibrium state. This paper conducts a brief review of research on the flow instability of nanofluids, including hydrodynamic instability and thermal instability. Some open questions on the subject are also identified. Key words nanofluid, thermal instability, hydrodynamic instability, review Chinese Library Classification O358, O359 2010 Mathematics Subject Classification 76E09, 76T20 1 Introduction Nanofluids have aroused significant interest over the past few decades for their wide applica- tions in energy, machinery, transportation, and healthcare. For example, low concentration of particles causes viscosity changes[1–2], decreases viscosity with increasing shear rate[3], changes friction factors and pressure drops[4–6], and improves heat transfer[7–9]. Moreover, the unique flow properties of nanofluids are determined by the flow pattern. Heat transfer[10] and pressure drop[11] are also much lower and higher, respectively, in laminar flow than in turbulent flow. By adding particles to the fluid, the thermal entropy generation and friction are of the same order of magnitude as in turbulent flow, while the effect of heat transfer entropy generation strongly outweighs that of the friction entropy generation in laminar flow. -
Suspensions of Finite-Size Rigid Particles in Laminar and Turbulent
Suspensions of finite-size rigid particles in laminar and turbulentflows by Walter Fornari November 2017 Technical Reports Royal Institute of Technology Department of Mechanics SE-100 44 Stockholm, Sweden Akademisk avhandling som med tillst˚andav Kungliga Tekniska H¨ogskolan i Stockholm framl¨agges till offentlig granskning f¨or avl¨aggande av teknologie doctorsexamenfredagen den 15 December 2017 kl 10:15 i sal D3, Kungliga Tekniska H¨ogskolan, Lindstedtsv¨agen 5, Stockholm. TRITA-MEK Technical report 2017:14 ISSN 0348-467X ISRN KTH/MEK/TR-17/14-SE ISBN 978-91-7729-607-2 Cover: Suspension offinite-size rigid spheres in homogeneous isotropic turbulence. c Walter Fornari 2017 � Universitetsservice US–AB, Stockholm 2017 “Considerate la vostra semenza: fatti non foste a viver come bruti, ma per seguir virtute e canoscenza.” Dante Alighieri, Divina Commedia, Inferno, Canto XXVI Suspensions offinite-size rigid particles in laminar and tur- bulentflows Walter Fornari Linn´eFLOW Centre, KTH Mechanics, Royal Institute of Technology SE-100 44 Stockholm, Sweden Abstract Dispersed multiphaseflows occur in many biological, engineering and geophysical applications such asfluidized beds, soot particle dispersion and pyroclastic flows. Understanding the behavior of suspensions is a very difficult task. Indeed particles may differ in size, shape, density and stiffness, their concentration varies from one case to another, and the carrierfluid may be quiescent or turbulent. When turbulentflows are considered, the problem is further complicated by the interactions between particles and eddies of different size, ranging from the smallest dissipative scales up to the largest integral scales. Most of the investigations on this topic have dealt with heavy small particles (typically smaller than the dissipative scale) and in the dilute regime. -
Advection Diffusion Model for Particles Deposition in Rayleigh-Bénard Turbulent Flows
International Conference Nuclear Energy for New Europe 2005 Bled, Slovenia, September 5-8, 2005 Advection Diffusion Model for Particles Deposition in Rayleigh-Bénard Turbulent Flows Paolo Oresta, Antonio Lippolis DIASS – Politecnico di Bari Viale del Turismo 8, 74100 Taranto, Italia [email protected], [email protected] Roberto Verzicco DIMeG and CEMeC – Politecnico di Bari Via Re David, 200, 70125 Bari, Italia [email protected] Alfredo Soldati DEM and CIFI – Università degli Studi di Udine Via delle Scienze, 208, 33100 Udine, Italia [email protected] ABSTRACT In this paper, Direct Numerical Simulation (DNS) and Lagrangian Particle Tracking are used to precisely investigate the turbulent thermally driven flow and particles dispersion in a closed, slender cylindrical domain. The numerical simulations are carried out for Rayleigh (Ra) and Prandtl numbers (Pr) equal to Ra = 2·108 and Pr = 0.7, considering three sets of particles with Stokes numbers, based on Kolmogorov scale, equal to Stk = 1.3, Stk = 0.65 and Stk = 0.13. This data are used to calculate a priori the drift velocity and the turbulent diffusion coefficient for the Advection Diffusion model. These quantities are function of the Stokes, Froude, Rayleigh and Prandtl numbers only. One dimensional, time dependent, Advection- Diffusion Equation (ADE) is presented to predict particles deposition in Rayleigh-Bénard flow in the cylindrical domain. This archetype configuration models flow and aerosol dynamics, produced in case of accident in the passive containment cooling system (PCCS) of a nuclear reactor. ADE results show a good agreement with DNS data for all the sets of particles investigated. 1 INTRODUCTION The passive containment cooling system (PCCS) consists of an inner steel shell and an outer concrete shell [1]. -
Dimensional Analysis and Modeling
cen72367_ch07.qxd 10/29/04 2:27 PM Page 269 CHAPTER DIMENSIONAL ANALYSIS 7 AND MODELING n this chapter, we first review the concepts of dimensions and units. We then review the fundamental principle of dimensional homogeneity, and OBJECTIVES Ishow how it is applied to equations in order to nondimensionalize them When you finish reading this chapter, you and to identify dimensionless groups. We discuss the concept of similarity should be able to between a model and a prototype. We also describe a powerful tool for engi- I Develop a better understanding neers and scientists called dimensional analysis, in which the combination of dimensions, units, and of dimensional variables, nondimensional variables, and dimensional con- dimensional homogeneity of equations stants into nondimensional parameters reduces the number of necessary I Understand the numerous independent parameters in a problem. We present a step-by-step method for benefits of dimensional analysis obtaining these nondimensional parameters, called the method of repeating I Know how to use the method of variables, which is based solely on the dimensions of the variables and con- repeating variables to identify stants. Finally, we apply this technique to several practical problems to illus- nondimensional parameters trate both its utility and its limitations. I Understand the concept of dynamic similarity and how to apply it to experimental modeling 269 cen72367_ch07.qxd 10/29/04 2:27 PM Page 270 270 FLUID MECHANICS Length 7–1 I DIMENSIONS AND UNITS 3.2 cm A dimension is a measure of a physical quantity (without numerical val- ues), while a unit is a way to assign a number to that dimension. -
On Dimensionless Numbers
chemical engineering research and design 8 6 (2008) 835–868 Contents lists available at ScienceDirect Chemical Engineering Research and Design journal homepage: www.elsevier.com/locate/cherd Review On dimensionless numbers M.C. Ruzicka ∗ Department of Multiphase Reactors, Institute of Chemical Process Fundamentals, Czech Academy of Sciences, Rozvojova 135, 16502 Prague, Czech Republic This contribution is dedicated to Kamil Admiral´ Wichterle, a professor of chemical engineering, who admitted to feel a bit lost in the jungle of the dimensionless numbers, in our seminar at “Za Plıhalovic´ ohradou” abstract The goal is to provide a little review on dimensionless numbers, commonly encountered in chemical engineering. Both their sources are considered: dimensional analysis and scaling of governing equations with boundary con- ditions. The numbers produced by scaling of equation are presented for transport of momentum, heat and mass. Momentum transport is considered in both single-phase and multi-phase flows. The numbers obtained are assigned the physical meaning, and their mutual relations are highlighted. Certain drawbacks of building correlations based on dimensionless numbers are pointed out. © 2008 The Institution of Chemical Engineers. Published by Elsevier B.V. All rights reserved. Keywords: Dimensionless numbers; Dimensional analysis; Scaling of equations; Scaling of boundary conditions; Single-phase flow; Multi-phase flow; Correlations Contents 1. Introduction ................................................................................................................. -
Dimensional Analysis and Modeling
cen72367_ch07.qxd 10/29/04 2:27 PM Page 269 CHAPTER DIMENSIONAL ANALYSIS 7 AND MODELING n this chapter, we first review the concepts of dimensions and units. We then review the fundamental principle of dimensional homogeneity, and OBJECTIVES Ishow how it is applied to equations in order to nondimensionalize them When you finish reading this chapter, you and to identify dimensionless groups. We discuss the concept of similarity should be able to between a model and a prototype. We also describe a powerful tool for engi- ■ Develop a better understanding neers and scientists called dimensional analysis, in which the combination of dimensions, units, and of dimensional variables, nondimensional variables, and dimensional con- dimensional homogeneity of equations stants into nondimensional parameters reduces the number of necessary ■ Understand the numerous independent parameters in a problem. We present a step-by-step method for benefits of dimensional analysis obtaining these nondimensional parameters, called the method of repeating ■ Know how to use the method of variables, which is based solely on the dimensions of the variables and con- repeating variables to identify stants. Finally, we apply this technique to several practical problems to illus- nondimensional parameters trate both its utility and its limitations. ■ Understand the concept of dynamic similarity and how to apply it to experimental modeling 269 cen72367_ch07.qxd 10/29/04 2:27 PM Page 270 270 FLUID MECHANICS Length 7–1 ■ DIMENSIONS AND UNITS 3.2 cm A dimension is a measure of a physical quantity (without numerical val- ues), while a unit is a way to assign a number to that dimension. -
Modeling Droplet Dispersion and Interphase Turbulent Kinetic Energy Transfer Using a New Dual-Timescale Langevin Model
International Journal of Multiphase Flow 33 (2007) 252–281 www.elsevier.com/locate/ijmulflow Modeling droplet dispersion and interphase turbulent kinetic energy transfer using a new dual-timescale Langevin model M.G. Pai, S. Subramaniam * Department of Mechanical Engineering, 3020, H.M. Black Engineering, Iowa State University, Ames, IA 50011, USA Received 19 May 2006; received in revised form 7 August 2006 Abstract Dispersion of spray droplets and the modulation of turbulence in the ambient gas by the dispersing droplets are two coupled phenomena that are closely linked to the evolution of global spray characteristics, such as the spreading rate of the spray and the spray cone angle. Direct numerical simulations (DNS) of turbulent gas flows laden with sub-Kol- mogorov size particles, in the absence of gravity, report that dispersion statistics and turbulent kinetic energy (TKE) evolve on different timescales. Furthermore, each timescale behaves differently with Stokes number, a non-dimensional flow parameter (defined in this context as the ratio of the particle response time to the Kolmogorov timescale of turbulence) that characterizes how quickly a particle responds to turbulent fluctuations in the carrier or gas phase. A new dual-time- scale Langevin model (DLM) composed of two coupled Langevin equations for the fluctuating velocities, one for each phase, is proposed. This model possesses a unique feature that the implied TKE and velocity autocorrelation in each phase evolve on different timescales. Consequently, this model has the capability of simultaneously predicting the disparate Stokes number trends in the evolution of dispersion statistics, such as velocity autocorrelations, and TKE in each phase. -
Three-Dimensional Buoyant Turbulent Flows in a Scaled Model, Slot-Ventilated, Livestock Conhnement Facility
THREE-DIMENSIONAL BUOYANT TURBULENT FLOWS IN A SCALED MODEL, SLOT-VENTILATED, LIVESTOCK CONHNEMENT FACILITY S. J. Hoff, K. A. Janni, L. D. Jacobson MEMBER MEMBER MEMBER ASAE ASAE ASAE ABSTRACT influences the velocity and temperature distributions A three-dimensional turbulence model was used to throughout the space. determine the effects of animal-generated buoyant forces Little information exists on velocity and temperature on the airflow patterns and temperature and airspeed distributions throughout a ventilated space beyond the distributions in a ceiling-slot, ventilated, swine grower inlet-jet-affected region. Spatial conditions generally have facility. The model incorporated the Lam-Bremhorst been described qualitatively based on overall airflow turbulence model for low-Reynolds Number airflow typical patterns. The microclimate of the animal, as a function of of slot-ventilated, livestock facilities. The predicted results the inlet conditions for winter conditions when the from the model were compared with experimental results potential for animal chilling is the greatest, is of prime from a scaled-enclosure. The predicted and measured concern. results indicated a rather strong cross-stream recirculation Mixed-flow ventilation research related to animal zone in the chamber that resulted in substantial three- confinement facilities has attempted to characterize the dimensional temperature distributions for moderate to desired inlet conditions based on the inlet jet behavior as it highly buoyancy-affected flows. Airflow patterns were enters the ventilated space. In the past, recommendations adequately predicted for Ar^ > 40 and J values < 0.00053. specified that the desired inlet velocity be maintained For Ar^ < 40 and J values > 0.00053, the visualized between 4.0 and 5.0 m/s.