DOCSLIB.ORG

Reynolds Number Effects on the Reynolds-Stress Budgets In

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Reynolds Number Effects on the Reynolds-Stress Budgets In PHYSICS OF FLUIDS 20, 101511 ͑2008͒ Reynolds number effects on the Reynolds-stress budgets in turbulent channels ͒ ͒ Sergio Hoyasa and Javier Jiménezb School of Aeronautics, Universidad Politécnica, 28040 Madrid, Spain ͑Received 28 December 2007; accepted 10 June 2008; published online 31 October 2008͒ Budgets for the nonzero components of the Reynolds-stress tensor are presented for numerical channels with Reynolds numbers in the range Re␶ =180–2000. The scaling of the different terms is + Ϸ discussed, both above and within the buffer and viscous layers. Above x2 150, most budget 3 4 components scale reasonably well with u␶ /h, but the scaling with u␶ /␯ is generally poor below that level. That is especially true for the dissipations and for the pressure-related terms. The former is traced to the effect of the wall-parallel large-scale motions, and the latter to the scaling of the pressure itself. It is also found that the pressure terms scale better near the wall when they are not separated into their diffusion and deviatoric components, but mostly only because the two terms tend to cancel each other in the viscous sublayer. The budgets, together with their statistical uncertainties, are available electronically from http://torroja.dmt.upm.es/channels. © 2008 American Institute of Physics. ͓DOI: 10.1063/1.3005862͔ I. INTRODUCTION nolds stress is found not to hold. As determinants, it is clear that failures in the scaling of the energy equations, or in the The interest of the budget equations for the normal and budget of the tangential Reynolds stress, bear directly on the tangential Reynolds stresses in turbulent shear flows extends dynamics of the flow. from their application in formulating Reynolds-averaged tur- The organization of this paper is as follows. The numeri- bulence models to the elucidation of the physics of the cas- cal data sets are introduced in Sec. II, followed by the estab- cade. This is especially true in wall-bounded turbulence, lishment of the notation for the budget equations. The scaling where inhomogeneity makes theoretical understanding par- of the budgets in the outer layers is described in Sec. IV, and ticularly challenging. Experimental difficulties prevented for the viscous and buffer layers are discussed in Sec. V. A final a long time the determination of many of the quantities in- section concludes. All the budgets discussed in this paper are volved, and it was not until the first direct numerical simu- available in Ref. 15. lation of a turbulent channel1 that reliable budgets of the Reynolds-stress tensor could be obtained.2 After that pioneer- ing paper, budgets have been published for other numerical flows,3–9 but they have usually been limited to relatively low II. THE NUMERICAL EXPERIMENTS Reynolds numbers by the resolution of the simulations. Most of the data used in this paper are from the turbulent The purpose of this paper is to introduce the Reynolds- channel simulations10–12 summarized in Table I. We use x stress budgets of a recent series of simulations of turbulent j and u , with j=1...3, for the streamwise, wall-normal, and channels covering a moderately wide Reynolds number j spanwise coordinates and velocity components, and the ki- range,10–12 and to discuss how they depend on the Reynolds nematic pressure p incorporates the constant fluid density. number. It was already noted in Ref. 2 that some dependence The density is also left out of the definition of the Reynolds was to be expected. It was not clear at the time in which stresses. The channel half width is h, and the + superindex direction, or for which range, although it soon became ap- denotes wall units, defined in terms of the friction velocity u␶ parent that the original data at Re␶ =180 were not represen- and of the kinematic viscosity ␯. Mean quantities are capi- tative of many of the features of higher Reynolds number talized, and lower-case symbols refer to fluctuations. Primed flows.9 It has been found since then that the classical scaling quantities refer to root-mean-squared ͑rms͒ fluctuation inten- in wall units of several flow properties near the wall holds + sities. The friction Reynolds number is Re␶ =h . only imperfectly, probably up to arbitrarily large Reynolds The numerical codes1 integrate the incompressible numbers,13,14 and it is interesting to examine how such scal- Navier–Stokes equations in the form of evolution problems ing failures influence the budget equations themselves. for the wall-normal vorticity ␻ and for the Laplacian of the The budget equations are relevant both as diagnostic and 2 wall-normal velocity, ٌ2u . The spatial discretization uses as dynamical quantities. As diagnostics, they give informa- 2 Fourier expansions in the wall-parallel planes, dealiased by tion on what has failed when the classical scaling of a Rey- the two-thirds rule. The three lowest Reynolds numbers use Chebychev polynomials in x , while the highest one uses a͒ 2 Present address: Univ. Politécnica de Valencia, CMT Motores Térmicos, seven-point compact finite differences. The characteristics of 46022 Valencia, Spain. ͒ b Also at Center for Turbulence Research, Stanford University. Electronic the different simulations with respect to the large scales are mail: [email protected]. documented in the original publications. Their resolution 1070-6631/2008/20͑10͒/101511/8/$23.0020, 101511-1 © 2008 American Institute of Physics Downloaded 31 Oct 2008 to 83.53.251.224. Redistribution subject to AIP license or copyright; see http://pof.aip.org/pof/copyright.jsp 101511-2 S. Hoyas and J. Jiménez Phys. Fluids 20, 101511 ͑2008͒ TABLE I. Parameters of the simulations. L1 and L3 are the periodic streamwise and spanwise dimensions of the ⌬ ⌬ numerical box, and h is the channel half width. 1 and 3 are the resolutions in terms of Fourier modes. N2 is the number of wall-normal collocation points. NF is the number of fields used for the statistics, and T is their time span. / / ⌬+ ⌬+ / Case Line Re␶ L1 hL3 h 1 3 N2 NF u␶T h ␲ ␲ L180 ¯¯·· 186 12 4 9 6.7 97 106 63 L550 —·— 547 8␲ 4␲ 13 6.7 257 149 22 L950 ---- 934 8␲ 3␲ 11 5.7 385 74 12 L2000 — 2003 8␲ 3␲ 12 6.1 633 226 11 properties regarding the smallest scales are discussed in Note that homogeneity along the two wall-parallel direc- Ref. 16. tions implies that some terms in Eq. ͑1͒ vanish identically for ␧ Because of minor bugs discovered in L550 and L950 equilibrium channels. Note also that the definitions of K and after the original runs, their statistics have been recomputed VK are in part interchangeable, and that the decomposition by rerunning with a clean code each of the several hundred used above is not the “thermodynamically correct” one.18 stored fields, long enough for their statistics near the wall to However, it is known that the difference between the two stabilize. The occasion was used to extend L550, for which definitions is negligible everywhere for low Reynolds num- relatively few fields had been stored, by several extra eddy ber channels,19 and the same is true for the present ones. turnovers, and to compute the budgets presented here. The difference between the new and the older statistics was found IV. THE OUTER LAYERS + Ϸ to be negligible except below x2 1, which was the location of the most important bug. The statistics of L180 and L2000 Away from the buffer layer, the basic scaling of all the ͑ ͒ / 3 / terms in Eq. 1 at a fixed x2 h is u␶ h. In an ideal logarith- were, as far as we know, bug-free. The behaviors of the 2 turbulent intensities and of the spectra in the buffer layer are mic layer, the tangential Reynolds stress would be u␶, and /␬ ␬ discussed in the original publications for the individual simu- U1,2=u␶ x2, where is the Kármán constant so that the 3 /␬ lations, and those in the logarithmic and outer layers are kinetic energy production would be u␶ x2. As a conse- quence, it can be expected that all the terms in Eq. ͑1͒ should further discussed in Ref. 17. −1 decrease away from the wall roughly as x2 , and it is conve- nient to represent them premultiplied by x2, as in Fig. 1. With III. THE BUDGET EQUATIONS the logarithmic abscissa used in that figure, this has the added advantage of making areas proportional to the inte- Following Ref. 2, the budget equation for the component −1 grated energy. Note that the x2 behavior holds reasonably ͗u u ͘ of the Reynolds-stress tensor is written as + Ϸ ͑ / i j well for all the budgets in Fig. 1, from x2 50 x2 h Ϸ ͒ / Ϸ B ϵ D͗u u ͘/Dt = P + ␧ + T + ⌸s + ⌸d + V , ͑1͒ 0.025 to x2 h 0.4. ij i j ij ij ij ij ij ij In agreement with previous results,2 all the budgets where ͗͘ stands for averaging over the two homogeneous above the buffer layer are dominated by a few terms. Energy directions and time. The different terms in the right-hand enters the flow through the streamwise velocity fluctuations, side of Eq. ͑1͒ are referred to as production, dissipation, from where it is extracted by the dissipation and by the turbulent diffusion, pressure-strain, pressure diffusion, and pressure-strain term. The pressure redistributes the energy to viscous diffusion, and are defined as u2 and u3, from where it is dissipated. All the other terms are / Ϸ P =−͗u u ͘U − ͗u u ͘U , ͑2͒ small except above x2 h 0.4, where the production de- ij i k j,k j k i,k creases because the mean velocity profile flattens, and the ␧ =−2␯͗u u ͘, ͑3͒ dissipation and redistribution terms are compensated by the ij i,k j,k turbulent and pressure diffusions.
Load more

Recommended publications
  • CFD-Driven Symbolic Identification of Algebraic Reynolds-Stress Models
    CFD-driven Symbolic Identification of Algebraic Reynolds-Stress Models Isma¨ılBEN HASSAN SA¨IDIa,∗, Martin SCHMELZERb, Paola CINNELLAc, Francesco GRASSOd aInstitut A´erotechnique, CNAM, 15 Rue Marat, 78210 Saint-Cyr-l'Ecole,´ France bFaculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 2, Delft, The Netherlands cInstitut Jean Le Rond D'Alembert, Sorbonne Universit´e,4 Place Jussieu, 75005 Paris, France dLaboratoire DynFluid, CNAM, 151 Boulevard de l'Hopital, 75013 Paris, France Abstract A CFD-driven deterministic symbolic identification algorithm for learning ex- plicit algebraic Reynolds-stress models (EARSM) from high-fidelity data is de- veloped building on the CFD-free SpaRTA algorithm of [1]. Corrections for the Reynolds stress tensor and the production of transported turbulent quantities of a baseline linear eddy viscosity model (LEVM) are expressed as functions of tensor polynomials selected from a library of candidate functions. The CFD- driven training consists in solving a blackbox optimization problem in which the fitness of candidate EARSM models is evaluated by running RANS simula- tions. A preliminary sensitivity analysis is used to identify the most influential terms and to reduce the dimensionality of the search space and the Constrained Optimization using Response Surface (CORS) algorithm, which approximates the black-box cost function using a response surface constructed from a limited number of CFD solves, is used to find the optimal model parameters within a realizable search space. The resulting turbulence models are numerically robust and ensure conservation of mean kinetic energy. Furthermore, the CFD-driven procedure enables training of models against any target quantity of interest com- putable as an output of the CFD model.
    [Show full text]
  • Turbulence Momentum Transport and Prediction of the Reynolds Stress in Canonical Flows
    Turbulence Momentum Transport and Prediction of the Reynolds Stress in Canonical Flows T.-W. Lee Mechanical and Aerospace Engineering, Arizona State University, Tempe, AZ, 85287 Abstract- We present a unique method for solving for the Reynolds stress in turbulent canonical flows, based on the momentum balance for a control volume moving at the local mean velocity. A differential transform converts this momentum balance to a solvable form. Comparisons with experimental and computational data in simple geometries show quite good agreements. An alternate picture for the turbulence momentum transport is offered, as verified with data, where the turbulence momentum is transported by the mean velocity while being dissipated by viscosity. The net momentum transport is the Reynolds stress. This turbulence momentum balance is verified using DNS and experimental data. T.-W. Lee Mechanical and Aerospace Engineering, SEMTE Arizona State University Tempe, AZ 85287-6106 Email: [email protected] 0 Nomenclature C1 = constants Re = Reynolds number based on friction velocity U = mean velocity in the x direction Ue = free-stream velocity V = mean velocity in the y direction u’ = fluctuation velocity in the x direction urms’ = root-mean square of u’ u’v’ = Reynolds stress = boundary layer thickness m = modified kinematic viscosity Introduction Finding the Reynolds stress has profound implications in fluid physics. Many practical flows are turbulent, and require some method of analysis or computations so that the flow process can be understood, predicted and controlled. This necessity led to several generations of turbulence models including a genre that models the Reynolds stress components themselves, the Reynolds stress models [1, 2].
    [Show full text]
  • A Mixing-Length Formulation for the Turbulent Prandtl Number in Wall-Bounded flows with Bed Roughness and Elevated Scalar Sources ͒ John P
    PHYSICS OF FLUIDS 18, 095102 ͑2006͒ A mixing-length formulation for the turbulent Prandtl number in wall-bounded flows with bed roughness and elevated scalar sources ͒ John P. Crimaldia Department of Civil, Environmental, and Architectural Engineering, University of Colorado, Boulder, Colorado 80309-0428 Jeffrey R. Koseff and Stephen G. Monismith Department of Civil and Environmental Engineering, Stanford University, Stanford, California 94305-4020 ͑Received 7 November 2005; accepted 20 June 2006; published online 5 September 2006͒ Turbulent Prandtl number distributions are measured in a laboratory boundary layer flow with bed roughness, active blowing and sucking, and scalar injection near the bed. The distributions are significantly larger than unity, even at large distances from the wall, in apparent conflict with the Reynolds analogy. An analytical model is developed for the turbulent Prandtl number, formulated as the ratio of momentum and scalar mixing length distributions. The model is successful at predicting the measured turbulent Prandtl number behavior. Large deviations from unity are shown in this case to be consistent with measurable differences in the origins of the momentum and scalar mixing length distributions. Furthermore, these deviations are shown to be consistent with the Reynolds analogy when the definition of the turbulent Prandtl number is modified to include the effect of separate mixing length origin locations. The results indicate that the turbulent Prandtl number for flows over complex boundaries can be modeled based on simple knowledge of the geometric and kinematic nature of the momentum and scalar boundary conditions. © 2006 American Institute of Physics. ͓DOI: 10.1063/1.2227005͔ I. INTRODUCTION For flows over rough surfaces, the nature of the roughness 9 has been shown to only slightly alter Prt.
    [Show full text]
  • 7. Turbulence Turbulent Jet
    7. Turbulence Turbulent Jet Instantaneous Mean Turbulent Boundary Layer y U(y) Instantaneous Mean What is Turbulence? • A “random”, 3-d, time-dependent eddying motion with many scales, superposed on an often drastically simpler mean flow • A solution of the Navier-Stokes equations • The natural state at high Reynolds numbers • An efficient transporter and mixer • A major source of energy loss • A significant influence on drag: ‒ increases frictional drag in non-separated flow ‒ delays, or sometimes prevents, boundary-layer separation on curved surfaces, so reducing pressure drag. ● “The last great unsolved problem of classical physics” Momentum Transfer in Laminar and Turbulent Flow • Laminar: ‒ smooth ‒ no mixing of fluid ‒ momentum transfer by viscous forces • Turbulent: ‒ chaotic ‒ mixing of fluid ‒ momentum transfer mainly by the net effect of intermingling ρ푈퐿 푈퐿 Regime determined by Reynolds number: Re = = μ ν “Low” Re laminar; “high” Re turbulent “High” or “low” depends on the flow and the choice of 푈 and 퐿 Reynolds’ Decomposition v u + mean fluctuation 푢 = 푢ത + 푢′ 푣 = 푣ҧ + 푣′ 푝 = 푝ҧ + 푝′ Alternative Notations • Overbar for mean, prime for fluctuation: 푢 + 푢′ −ρ푢′푣′ • Upper case for mean, lower case for fluctuation: 푈 + 푢 −ρ푢푣 Reynolds Averaging of a Product 푢 = 푢 + 푢′ 푢′ = 0 cf statistics: σ 푢2 2 2 ′2 σ2 = 푢′2 = − 푢ത2 푢 = 푢 + 푢 Variance 푁 σ 푢푣 푢푣 = 푢 푣 + 푢′푣′ ρ ≡ 푢′푣′ = − 푢ത푣ҧ Covariance 푁 푢푣 = (푢 + 푢′)(푣 + 푣′) = 푢 푣 + 푢푣′ + 푢′푣 + 푢′푣′ 푢푣 = 푢 푣 + 푢푣ഥ′ + 푢ഥ′푣 + 푢′푣′ 푢푣 = 푢 푣 + 푢′푣′ Effect of Turbulence on the Mean Flow (i) Mass vA Mass flux: ρ푣퐴 Average mass flux: ρ푣퐴 The mean velocity satisfies the same continuity equation as the instantaneous velocity Effect of Turbulence on the Mean Flow (ii) Momentum vA (푥-)momentum flux: (ρ푣퐴)푢 = ρ(푢푣)퐴 u Average momentum flux : (ρ푣퐴)푢 = ρ(푢 푣 + 푢′푣′)퐴 extra term Net rate of transport of momentum per unit area ρ푢′푣′ from LOWER to UPPER ..
    [Show full text]
  • Intrinsic Plasma Rotation and Reynolds Stress at the Plasma
    Measurements of Reynolds Stress and its Contribution to the Momentum Balance in the HSX Stellarator by Robert S. Wilcox A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy (Electrical Engineering) at the University of Wisconsin–Madison 2014 Date of final oral examination: 12/2/2014 The dissertation is approved by the following members of the Final Oral Committee: David T. Anderson, Professor, Electrical Engineering Amy E. Wendt, Professor, Electrical Engineering Chris C. Hegna, Professor, Engineering Physics Paul W. Terry, Professor, Physics Joseph N. Talmadge, Associate Scientist, Electrical Engineering c Copyright by Robert S. Wilcox 2014 All Rights Reserved i ABSTRACT In a magnetic configuration that has been sufficiently optimized for quasi-symmetry, the neoclas- sical transport and viscosity can be small enough that other terms can compete in the momentum balance to determine the plasma rotation and radial electric field. The Reynolds stress generated by plasma turbulence is identified as the most likely candidate for non-neoclassical flow drive in the HSX stellarator. Using multi-tipped Langmuir probes in the edge of HSX in the quasi-helically symmetric (QHS) configuration, the radial electric field and parallel flows are found to deviate from the values calculated by the neoclassical transport code PENTA using the ambipolarity con- straint in the absence of externally injected momentum. The local Reynolds stress in the parallel and perpendicular directions on a surface is also measured using the fluctuating components of floating potential and ion saturation current measurements. Although plasma turbulence enters the momentum balance as the flux surface averaged radial gradient of the Reynolds stress, the locally measured quantity implies a significant contribution to the momentum balance.
    [Show full text]
  • Computational Fluid Dynamics Techniques for Flows in Lapple Cyclone Separator
    COMPUTATIONAL FLUID DYNAMICS TECHNIQUES FOR FLOWS IN LAPPLE CYCLONE SEPARATOR A. F. Lacerda, L. G. M.Vieira, A. M. Nascimento, S. D. Nascimento, J. J. R. Damasceno and M. A. S. Barrozo. Federal University of Uberlândia, Faculty of Chemical Engineering -FEQUI, Block K, Campus Santa Mônica, Uberlândia-MG - Brazil. ZIP: 38400-902 – Fax: 55-034-32394188 E-mail: [email protected] Keywords: Separation; Lapple; Cyclones; Computational Fluid Dynamics; Fluent Abstract A two-dimensional fluidynamics model for turbulent flow of gas in cyclones is used for available the importance of the anisotropic of the Reynolds stress components. This study presents consisted in to simulate through computational fluid dynamics (CFD) package the operation of the Lapple cyclone. Yields of velocity obtained starting from a model anisotropic of the Reynolds stress are compared with experimental data of the literature, as form of validating the results obtained through the use of the Computational fluid dynamics (Fluent). The experimental data of the axial and swirl velocities validate numeric results obtained by the model. 1 - Introduction Cyclones are equipment used for the separation and suspended solid collection in gaseous chains. Its popularity if must mainly to the its simplicity of construction, absence of mobile parts, what it guarantees a low necessity of maintenance. Cyclones are among the oldest of industrial particulate control equipment and air sampling device. The primary advantages of cyclones are economy and simplicity in construction and designs. By using suitable materials and methods of construction, cyclones may be adapted for use in extreme operating conditions: high temperature, high pressure, and corrosive gases. Therefore, cyclones have found increasing utility in the field of air pollution [1].
    [Show full text]
  • On Reynolds Stresses and Turbulent Flows in Circular Ducts
    ON REYNOLDS STRESSES AND TURBULENT FLOWS IN CIRCULAR DUCTS A THESIS Presented to The Faculty of the Division of Graduate Studies and Research . *y • Kenneth Alan Williams In Partial Fulfillment of the Requirements for the Degree Master of Science in Mechanical Engineering Georgia Institute of Technology June, 1974 ON REYNOLDS STRESSES AND TURBULENT FLOWS IN CIRCULAR DUCTS Approved: Novak Zuber, Chairman Ward 0. Winer /f) ~ K PV^V. Desai- Charles W. Gorton Date approved by Chairman: ""7 7 ' ^ / 11 ACKNOWLEDGMENTS The author wishes to express his deep appreciation to his advisor, Dr. Novak Zuber, for suggesting the thesis area and for his devoted assistance which made the success of this work possible. The author is also grateful for the valuable career guidance given him by his advisor. It is a pleasure to thank Drs. Winer and Desai of the School of Mechanical Engineering and Dr. Gorton of the School of Chemical Engineering, for their interest in the work and for their meaningful comments and suggestions. Finally the author wishes to express his gratitude toward his entire family, whose continued encouragement and support made his education possible. TABLE OF CONTENTS Page ACKNOWLEDGMENTS. ..... .... ... ii LIST OF ILLUSTRATIONS. .,. ,-. • • • • v NOMENCLATURE . „ . .... .., ..... vi SUMMARY. ..... ........ ... ..... viii Chapter I. INTRODUCTION. .... ... ..... 1 1.1 Significance of the Problem 1.2 Purpose of the Tlvesas II. BASIC FORMULATION AND DISCUSSION . ... 2 2.1 Analytical Formulation of Basic Relationships 2; 1.1 Shear. Stress Distribution 2.1.2 Reynolds Equation 2.1.3 Closure Problem 2.2 Present Methods 2.3 General Observations Concerning Turbulent Flows 2.4 Comments and Conclusions III.
    [Show full text]
  • Reynolds Averaged Navier Stokes Equations and It Is Usually Called As RANS
    Simulations for Enhancing Aerodynamic Designs 2. Governing Equations and Turbulence Models by Dr. KANNAN B T, M.E (Aero), M.B.A (Airline & Airport), PhD (Aerospace Engg), Grad.Ae.S.I, M.I.E, M.I.A.Eng, M.I.A.CS.IT, Conservation Laws ➢ Conservation of mass “Rate of increase of mass in a fluid element equals net rate of flow of mass into a fluid element” ➢ Conservation of Momentum “Rate of increase of momentum of fluid particle equals sum of forces acting on fluid particle” ➢ Conservation of Energy “Rate of increase of energy of fluid particle equals sum of net rate of heat added to fluid particle and net rate of work done on fluid particle” ✔ Scalar Transport It deals with the transport of active and passive scalars. Governing Equations for Turbulent Flows Instantaneous equations ↓ Reynolds Decomposition Decomposed equations ↓ Reynolds Averaging Reynolds Averaged Equations Reynolds Decomposition Instantaneous velocity = Mean velocity + Fluctuating velocity Averaging RANS Navier Stokes Equations subjected to Reynolds Decomposition and Reynolds Averaging yields Reynolds Averaged Navier Stokes Equations and it is usually called as RANS. Instantaneous Governing Equations Reynolds Mean Momentum Equation RANS CLOSURE RANS = Mean momentum equation having Reynolds Stress / Apparent Mean Stress as additional term which was generated by the averaging process. Hence, Number of unknowns > Number of equations ↓ CLOSURE PROBLEM OF TURBULENCE Solution: Modeling for the unknown New Unknown The closure problem is due to Reynolds Stress resulting from the non-linear term from Navier Stokes equations. This non-linear term is responsible for the energy cascading. Energy transfer takes place by “ENERGY CASCADE” Reynolds Stress The Reynolds Stress (RS) is defined by the Tensor <uv> or <uiuj> or <u’v’>.
    [Show full text]
  • Analytical Models of Velocity, Reynolds Stress and Turbulence Intensity in Ice-Covered Channels
    water Article Analytical Models of Velocity, Reynolds Stress and Turbulence Intensity in Ice-Covered Channels Jiao Zhang 1, Wen Wang 1,*, Zhanbin Li 1, Qian Li 2, Ya Zhong 3, Zhaohui Xia 4 and Hunan Qiu 1 1 State Key Laboratory of Eco-Hydraulics in Northwest Arid Region of China, Xi’an University of Technology, Xi’an 710048, China; [email protected] (J.Z.); [email protected] (Z.L.); [email protected] (H.Q.) 2 Yellow River Engineering Consulting Co., Ltd., Zhengzhou 450003, China; [email protected] 3 Southwest Branch of China Construction Third Engineering Bureau Group Co., Ltd., Chengdu 610041, China; [email protected] 4 PowerChina Northwest Engineering Corporation Limited, Xi’an 710065, China; [email protected] * Correspondence: [email protected] Abstract: Ice cover in an open channel can influence the flow structure, such as the flow velocity, Reynolds stress and turbulence intensity. This study analyzes the vertical distributions of velocity, Reynolds stress and turbulence intensity in fully and partially ice-covered channels by theoretical methods and laboratory experiments. According to the experimental data, the vertical profile of longitudinal velocities follows an approximately symmetry form. Different from the open channel flow, the maximum value of longitudinal velocity occurs near the middle of the water depth, which is close to the channel bed with a smoother boundary roughness compared to the ice cover. The measured Reynolds stress has a linear distribution along the vertical axis, and the vertical distribution of measured turbulence intensity follows an exponential law. Theoretically, a two-power-law function is presented to obtain the analytical formula of the longitudinal velocity.
    [Show full text]
  • Optimal Fluxes and Reynolds Stresses
    J. Fluid Mech. (2016), vol. 809, pp. 585–600. c Cambridge University Press 2016 585 doi:10.1017/jfm.2016.692 Optimal fluxes and Reynolds stresses Javier Jiménez† School of Aeronautics, Universidad Politécnica de Madrid, 28040 Madrid, Spain (Received 6 June 2016; revised 11 September 2016; accepted 20 October 2016) It is remarked that fluxes in conservation laws, such as the Reynolds stresses in the momentum equation of turbulent shear flows, or the spectral energy flux in anisotropic turbulence, are only defined up to an arbitrary solenoidal field. While this is not usually significant for long-time averages, it becomes important when fluxes are modelled locally in large-eddy simulations, or in the analysis of intermittency and cascades. As an example, a numerical procedure is introduced to compute fluxes in scalar conservation equations in such a way that their total integrated magnitude is minimised. The result is an irrotational vector field that derives from a potential, thus minimising sterile flux ‘circuits’. The algorithm is generalised to tensor fluxes and applied to the transfer of momentum in a turbulent channel. The resulting instantaneous Reynolds stresses are compared with their traditional expressions, and found to be substantially different. This suggests that some of the alleged shortcomings of simple subgrid models may be representational artefacts, and that the same may be true of the intermittency properties of the turbulent stresses. Key words: mathematical foundations, turbulence theory, turbulent boundary layers 1. Introduction Conservation laws are staples of continuum mechanics. They take the form of the rate of change of a conserved quantity ρ, such as mass, energy or momentum density, balanced by the divergence of a vector flux φ φ , D f jg @ ρ @ φ S; (1.1) t C j j D Q where @j is the partial derivative along the jth coordinate, repeated indices imply summation over all coordinate directions and SQ represents any sources or sinks.
    [Show full text]
  • Turbulence Closure Models for Computational Fluid Dynamics Paul A
    Aerospace Engineering Publications Aerospace Engineering 2-23-2018 Turbulence Closure Models for Computational Fluid Dynamics Paul A. Durbin Iowa State University, [email protected] Follow this and additional works at: https://lib.dr.iastate.edu/aere_pubs Part of the Aerodynamics and Fluid Mechanics Commons, and the Computational Engineering Commons The ompc lete bibliographic information for this item can be found at https://lib.dr.iastate.edu/ aere_pubs/136. For information on how to cite this item, please visit http://lib.dr.iastate.edu/ howtocite.html. This Book Chapter is brought to you for free and open access by the Aerospace Engineering at Iowa State University Digital Repository. It has been accepted for inclusion in Aerospace Engineering Publications by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. Turbulence Closure Models for Computational Fluid Dynamics Abstract The formulation of analytical turbulence closure models for use in computational fluid mechanics is described. The ubjs ect of this chapter is the types of models that are used to predict the statistically averaged flow field – commonly known as Reynolds‐averaged Navier–Stokes equations (RANS) modeling. A variety of models are reviewed: these include two‐equation, eddy viscosity transport, and second moment closures. How they are formulated is not the main theme; it enters the discussion but the models are presented largely at an operational level. Several issues related to numerical implementation are discussed. Relative merits of the various formulations are commented on. Keywords turbulence modeling, RANS, k ‐epsilon model, Reynolds stress transport, second moment closure, turbulence prediction methods Disciplines Aerodynamics and Fluid Mechanics | Aerospace Engineering | Computational Engineering Comments This is a chapter from Durbin, Paul A.
    [Show full text]
  • Analytical Methods for the Development of Reynolds-Stress Closures in Turbulence
    Annual Reviews www.annualreviews.org/aronline Annu. Rev. Fluid Mech. 1991.23 : 107-57 Copyright © 1991 by Annual Reviews Inc. All rights rexerved ANALYTICAL METHODS FOR THE DEVELOPMENT OF REYNOLDS-STRESS CLOSURES IN TURBULENCE Charles G. Speziale Institute for ComputerApplications in Science and Engineering, NASALangley Research Center, Hampton, Virginia 23665 KEYWORDS: turbulence modeling, K-e model, two-equation models, second- order closures INTRODUCTION Despite over a century of research, turbulence remains the major unsolved problem of classical physics. While most researchers agree that the basic physics of turbulence can be described by the Navier-Stokes equations, limitations in computer capacity make it impossible--for now and the foreseeable future--to directly solve these equations for the complextur- bulent flows of technological interest. Hence, virtually all scientific and engineering calculations of nontrivial turbulent flows, at high Reynolds by University of Utah - Marriot Library on 02/19/09. For personal use only. numbers, are based on some type of modeling. This modeling can take a variety of forms: Annu. Rev. Fluid Mech. 1991.23:107-157. Downloaded from arjournals.annualreviews.org 1. Reynolds-stress models, which allow for the calculation of one-point first and second momentssuch as the mean velocity, mean pressure, and turbulent kinetic energy; 2. subgrid-scale models for large-eddy simulations, wherein the large, energy-containing eddies are computed directly and the effect of the small scales--which are more universal in character--are modeled; 3. two-point closures or spectral models, which provide more detailed information about the turbulence structure, since they are based on the two-point velocity correlation tensor; or 107 0066-4189/91/0115-0107502.00 Annual Reviews www.annualreviews.org/aronline 108 SPEZIALE 4.
    [Show full text]