Turbulence Closure Models for Computational Fluid Dynamics Paul A

Total Page:16

File Type:pdf, Size:1020Kb

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. "Turbulence Closure Models for Computational Fluid Dynamics." In Encyclopedia of Computational Mechanics, Second Edition, edited by Erwin Stein, Ren de Borst and Thomas J. R. Hughes, 1-22. Chichester: John Wiley & Sons, 2018. DOI: 10.1002/9781119176817.ecm2061. Posted with permission. This book chapter is available at Iowa State University Digital Repository: https://lib.dr.iastate.edu/aere_pubs/136 Turbulence Closure Models for Computational Fluid Dynamics Paul A. Durbin Iowa State University, Ames, IA, USA of turbulent flow produces a reproducible, smooth flow field. 1 Introduction: The Role of Statistical Closure 1 Quantities such as the mean and variance of the velocity 2 Reynolds-Averaged Navier–Stokes Equations 1 provide definite values to be used in engineering analysis. It 3 Models with Scalar Variables 3 would seem that the smoother, averaged flow also is more amenable to computation than the instantaneous, random 4 Second Moment Transport 11 flow. Unfortunately, there are no exact equations governing 5 Reynolds-Averaged Computation 17 this smooth, average field. This is where closure modeling, References 21 the subject of this chapter, comes into play. For historical reasons, the mean velocity is called the Reynolds-averaged velocity and the equations obtained by averaging the Navier–Stokes equations are called the RANS 1 INTRODUCTION: THE ROLE OF (Reynolds-averaged Navier–Stokes) equations. Figure 1 STATISTICAL CLOSURE contrasts an instantaneous, random velocity field, to its ensemble average. The former is a direct numerical simu- Turbulence is the highly irregular flow of fluids. It lation; the latter is its Reynolds average. Statistical closure is governed by the exact, Navier–Stokes, momentum models are meant to predict the field shown in (b), without equations; but it is of little comfort to realize that turbulence having to average over an ensemble of fields shown in is just a particular type of solution to these laws of fluid (a). To accomplish this, new equations must be added to dynamics. Although its full disorderliness can be directly Navier–Stokes so that the average effects of turbulent mixing simulated on the computer (see Turbulence Direct Numer- are represented. These extra, turbulence closure equations, ical Simulation and Large-Eddy Simulation), that is too by necessity, contain empirical coefficients; this is not a expensive computationally and too fine a level of detail shortcoming, it is usually the only prospect one has to for many practical purposes. When the need is for timely obtain predictions of engineering accuracy with manageable prediction of the flow fields in practical devices, statistical computing times. moment closures of the type discussed in this chapter are invariably invoked. There are good reasons why most of the analytical approaches to turbulence prediction resort to statistical 2 REYNOLDS-AVERAGED descriptions. The average over an ensemble of realizations NAVIER–STOKES EQUATIONS Encyclopedia of Computational Mechanics Second Edition, The equations that underlie single point moment closure Edited by Erwin Stein, René de Borst and Thomas J.R. Hughes. models will be briefly summarized. Lengthy discussions of © 2017 John Wiley & Sons, Ltd. their derivation and interpretation can be found in texts on DOI: 10.1002/9781119176817.ecm2061 turbulence (Pope, 2000; Durbin and Reif, 2010). 2 Turbulence Closure Models for Computational Fluid Dynamics 4 where U ≡ ũ. The fluctuation u is defined to be the turbu- 3 lence. For variable density, a convenient formalism consists of the introduction of the density-weighted averages, U ≡ h ̃ ≡ / 2 u and uiuj uiuj. We will allow for density variation, y but we are not primarily concerned with direct effects of 1 compressibility on the turbulence. Ignoring compressibility in the turbulence equations, although not in the mean flow, 0 0 5 10 is generally acceptable well beyond transonic speeds (Barre (a) x/h et al., 2002). The turbulence problem, as presently formulated, is to 4 describe the statistics of the velocity field, without access 3 to realizations of the random flow. It seems sensible to start by attempting to derive equations for statistics. Toward this h / 2 end, averages of the Navier–Stokes equations can be formed, y in hopes of finding equations that govern the mean velocity, 1 the velocity covariances (uiuj), and so on. Regrettably, the 0 averaged equations are unclosed – meaning that each set 0 5 10 of statistical moment equations contains more unknowns (b) x /h than equations. In that sense, they fall short of any ambi- tion to arrive at governing laws for statistics. However, the Figure 1. U contours in a ribbed channel. (a) Instantaneous u field Reynolds-averaged equations give an insight into the factors (DNS) and (b) ensemble average (RANS). (Reproduced from Ikeda and Durbin (2002) courtesy of T. Ikeda. © Ikeda & Durbin, 2002.) that govern the evolution of the mean flow and Reynolds stresses; they also form the basis for the closure models to be discussed subsequently. We introduce the ensemble average of a random function The momentum and continuity equations governing f (x, t) (Newtonian) viscous flow, whether turbulent or laminar, are White (1991) ∑N , 1 , ′ ′ ′ ̃ ̃ ̃ ̃ ̃ ̃ f (x t) = lim fi(x t) or f = f P( f )df (1) t ui + j ujui =− ip + j[ ( iuj + jui)] N→∞ N ∫ i=1 ̃ t + j uj = 0(5) for either discrete samples or a continuous probability density. If the random process is statistically stationary, the If the Reynolds decomposition (4) is substituted into (5) and above can be replaced by a time average the result is averaged, the RANS equations t 1 U + U U =− P + [( U + U )] − ( u u ) f (x) = lim f (x; t′)dt′ (2) t i j j i i j i j j i j j i → ∫ t ∞ t 0 t + j Uj = 0(6) The caveat of statistical stationarity means that the statistics are independent of the time origin; in other words, f (t) and are obtained. The viscous term invokes an assumption that density fluctuations are not significant in viscous regions. f (t + t0) have the same statistical properties for any t0.Iff is statistically homogeneous in direction y, Equations (6) for the mean velocity are equivalent to equations (5) for the total instantaneous velocity, except for 1 y the last, highlighted, term of the momentum equation. This f = lim f (x, z, t; y′)dy′ (3) → ∫ y ∞ y 0 term is a derivative of the Reynolds stress tensor. It comes from the convective derivative, so the Reynolds stresses can be used, the result being independent of the direction of represent the averaged effect of turbulent convection. Any homogeneity, y. understanding of the nature of closure models relies on The Reynolds decomposition of the random variable, ũ,is recognizing that they represent this ensemble averaged into a sum of its mean and a fluctuation, effect, which, for instance, diffuses mean momentum. The mean flow equations (6) are unclosed because they ũ = U + u (4) contain six unknown components of the Reynolds stress Turbulence Closure Models for Computational Fluid Dynamics 3 tensor, uu. These derive from averaging the quadratic nonlin- transport of the Reynolds stress tensor. The first category earity of the Navier–Stokes equations. Any nonlinearity includes single equations for eddy viscosity and pairs of causes moment equations to be unclosed: here, the first equations for turbulent kinetic energy and its dissipation; the moment equation contains second moments; the second second category consists of methods based on the Reynolds moment equation will contain third moments; and so on up stress transport equation (7). the hierarchy. The second moment is
Recommended publications
  • Multiscale Computational Fluid Dynamics
    energies Review Multiscale Computational Fluid Dynamics Dimitris Drikakis 1,*, Michael Frank 2 and Gavin Tabor 3 1 Defence and Security Research Institute, University of Nicosia, Nicosia CY-2417, Cyprus 2 Department of Mechanical and Aerospace Engineering, University of Strathclyde, Glasgow G1 1UX, UK 3 CEMPS, University of Exeter, Harrison Building, North Park Road, Exeter EX4 4QF, UK * Correspondence: [email protected] Received: 3 July 2019; Accepted: 16 August 2019; Published: 25 August 2019 Abstract: Computational Fluid Dynamics (CFD) has numerous applications in the field of energy research, in modelling the basic physics of combustion, multiphase flow and heat transfer; and in the simulation of mechanical devices such as turbines, wind wave and tidal devices, and other devices for energy generation. With the constant increase in available computing power, the fidelity and accuracy of CFD simulations have constantly improved, and the technique is now an integral part of research and development. In the past few years, the development of multiscale methods has emerged as a topic of intensive research. The variable scales may be associated with scales of turbulence, or other physical processes which operate across a range of different scales, and often lead to spatial and temporal scales crossing the boundaries of continuum and molecular mechanics. In this paper, we present a short review of multiscale CFD frameworks with potential applications to energy problems. Keywords: multiscale; CFD; energy; turbulence; continuum fluids; molecular fluids; heat transfer 1. Introduction Almost all engineered objects are immersed in either air or water (or both), or make use of some working fluid in their operation.
    [Show full text]
  • 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]
  • Deep Learning Models for Turbulent Shear Flow
    DEGREE PROJECT IN MATHEMATICS, SECOND CYCLE, 30 CREDITS STOCKHOLM, SWEDEN 2018 Deep Learning models for turbulent shear flow PREM ANAND ALATHUR SRINIVASAN KTH ROYAL INSTITUTE OF TECHNOLOGY SCHOOL OF ENGINEERING SCIENCES Deep Learning models for turbulent shear flow PREM ANAND ALATHUR SRINIVASAN Degree Projects in Scientific Computing (30 ECTS credits) Degree Programme in Computer Simulations for Science and Engineering (120 credits) KTH Royal Institute of Technology year 2018 Supervisors at KTH: Ricardo Vinuesa, Philipp Schlatter, Hossein Azizpour Examiner at KTH: Michael Hanke TRITA-SCI-GRU 2018:236 MAT-E 2018:44 Royal Institute of Technology School of Engineering Sciences KTH SCI SE-100 44 Stockholm, Sweden URL: www.kth.se/sci iii Abstract Deep neural networks trained with spatio-temporal evolution of a dy- namical system may be regarded as an empirical alternative to conven- tional models using differential equations. In this thesis, such deep learning models are constructed for the problem of turbulent shear flow. However, as a first step, this modeling is restricted to a simpli- fied low-dimensional representation of turbulence physics. The train- ing datasets for the neural networks are obtained from a 9-dimensional model using Fourier modes proposed by Moehlis, Faisst, and Eckhardt [29] for sinusoidal shear flow. These modes were appropriately chosen to capture the turbulent structures in the near-wall region. The time series of the amplitudes of these modes fully describe the evolution of flow. Trained deep learning models are employed to predict these time series based on a short input seed. Two fundamentally different neural network architectures, namely multilayer perceptrons (MLP) and long short-term memory (LSTM) networks are quantitatively compared in this work.
    [Show full text]
  • Development of a Wake Model for Wind Farms Based on an Open Source CFD Solver
    Development of a wake model for wind farms based on an open source CFD solver. Strategies on parabolization and turbulence modeling PhD Thesis Daniel Cabezón Martínez Departamento de Ingeniería Energética y Fluidomecánica, Escuela Técnica Superior de Ingenieros Industriales, Universidad Politécnica de Madrid (UPM), Madrid, Spain Abstract Wake effect represents one of the most important aspects to be analyzed at the engineering phase of every wind farm since it supposes an important power deficit and an increase of turbulence levels with the consequent decrease of the lifetime. It depends on the wind farm design, wind turbine type and the atmospheric conditions prevailing at the site. Traditionally industry has used analytical models, quick and robust, which allow carry out at the preliminary stages wind farm engineering in a flexible way. However, new models based on Computational Fluid Dynamics (CFD) are needed. These models must increase the accuracy of the output variables avoiding at the same time an increase in the computational time. Among them, the elliptic models based on the actuator disk technique have reached an extended use during the last years. These models present three important problems in case of being used by default for the solution of large wind farms: the estimation of the reference wind speed upstream of each rotor disk, turbulence modeling and computational time. In order to minimize the consequence of these problems, this PhD Thesis proposes solutions implemented under the open source CFD solver OpenFOAM and adapted for each type of site: a correction on the reference wind speed for the general elliptic models, the semi-parabollic model for large offshore wind farms and the hybrid model for wind farms in complex terrain.
    [Show full text]
  • Simulation of Turbulent Flows
    Simulation of Turbulent Flows • From the Navier-Stokes to the RANS equations • Turbulence modeling • k-ε model(s) • Near-wall turbulence modeling • Examples and guidelines ME469B/3/GI 1 Navier-Stokes equations The Navier-Stokes equations (for an incompressible fluid) in an adimensional form contain one parameter: the Reynolds number: Re = ρ Vref Lref / µ it measures the relative importance of convection and diffusion mechanisms What happens when we increase the Reynolds number? ME469B/3/GI 2 Reynolds Number Effect 350K < Re Turbulent Separation Chaotic 200 < Re < 350K Laminar Separation/Turbulent Wake Periodic 40 < Re < 200 Laminar Separated Periodic 5 < Re < 40 Laminar Separated Steady Re < 5 Laminar Attached Steady Re Experimental ME469B/3/GI Observations 3 Laminar vs. Turbulent Flow Laminar Flow Turbulent Flow The flow is dominated by the The flow is dominated by the object shape and dimension object shape and dimension (large scale) (large scale) and by the motion and evolution of small eddies (small scales) Easy to compute Challenging to compute ME469B/3/GI 4 Why turbulent flows are challenging? Unsteady aperiodic motion Fluid properties exhibit random spatial variations (3D) Strong dependence from initial conditions Contain a wide range of scales (eddies) The implication is that the turbulent simulation MUST be always three-dimensional, time accurate with extremely fine grids ME469B/3/GI 5 Direct Numerical Simulation The objective is to solve the time-dependent NS equations resolving ALL the scale (eddies) for a sufficient time
    [Show full text]
  • ESSENTIALS of METEOROLOGY (7Th Ed.) GLOSSARY
    ESSENTIALS OF METEOROLOGY (7th ed.) GLOSSARY Chapter 1 Aerosols Tiny suspended solid particles (dust, smoke, etc.) or liquid droplets that enter the atmosphere from either natural or human (anthropogenic) sources, such as the burning of fossil fuels. Sulfur-containing fossil fuels, such as coal, produce sulfate aerosols. Air density The ratio of the mass of a substance to the volume occupied by it. Air density is usually expressed as g/cm3 or kg/m3. Also See Density. Air pressure The pressure exerted by the mass of air above a given point, usually expressed in millibars (mb), inches of (atmospheric mercury (Hg) or in hectopascals (hPa). pressure) Atmosphere The envelope of gases that surround a planet and are held to it by the planet's gravitational attraction. The earth's atmosphere is mainly nitrogen and oxygen. Carbon dioxide (CO2) A colorless, odorless gas whose concentration is about 0.039 percent (390 ppm) in a volume of air near sea level. It is a selective absorber of infrared radiation and, consequently, it is important in the earth's atmospheric greenhouse effect. Solid CO2 is called dry ice. Climate The accumulation of daily and seasonal weather events over a long period of time. Front The transition zone between two distinct air masses. Hurricane A tropical cyclone having winds in excess of 64 knots (74 mi/hr). Ionosphere An electrified region of the upper atmosphere where fairly large concentrations of ions and free electrons exist. Lapse rate The rate at which an atmospheric variable (usually temperature) decreases with height. (See Environmental lapse rate.) Mesosphere The atmospheric layer between the stratosphere and the thermosphere.
    [Show full text]
  • An Introduction to Turbulence Modeling for CFD
    An Introduction to Turbulence Modeling for CFD Gerald Recktenwald∗ February 19, 2020 ∗Mechanical and Materials Engineering Department Portland State University, Portland, Oregon, [email protected] Turbulence is a Hard Problem • Unsteady • Many length scales • Energy transfer between scales: ! Large eddies break up into small eddies • Steep gradients near the wall ME 4/548: Turbulence Modeling page 1 Engineering Model: Flow is \Steady-in-the-Mean" (1) 2 1.8 1.6 1.4 1.2 u 1 0.8 0.6 0.4 0.2 0 0 0.5 1 1.5 2 t ME 4/548: Turbulence Modeling page 2 Engineering Model: Flow is \Steady-in-the-Mean" (2) Reality: Turbulent flows are unsteady: fluctuations at a point are caused by convection of eddies of many sizes. As eddies move through the flow the velocity field changes in complex ways at a fixed point in space. Turbulent flows have structures { blobs of fluid that move and then break up. ME 4/548: Turbulence Modeling page 3 Engineering Model: Flow is \Steady-in-the-Mean" (3) Engineering Model: When measured with a \slow" sensor (e.g. Pitot tube) the velocity at a point is apparently steady. For basic engineering analysis we treat flow variables (velocity components, pressure, temperature) as time averages (or ensemble averages). These averages are steady (ignorning ensemble averaging of periodic flows). ME 4/548: Turbulence Modeling page 4 Engineering Model: Enhanced Transport (1) Turbulent eddies enhance mixing. • Transport in turbulent flow is much greater than in laminar flow: e.g. pollutants spread more rapidly in a turbulent flow than a laminar flow • As a result of enhanced local transport, mean profiles tend to be more uniform except near walls.
    [Show full text]
  • Hydraulics Manual Glossary G - 3
    Glossary G - 1 GLOSSARY OF HIGHWAY-RELATED DRAINAGE TERMS (Reprinted from the 1999 edition of the American Association of State Highway and Transportation Officials Model Drainage Manual) G.1 Introduction This Glossary is divided into three parts: · Introduction, · Glossary, and · References. It is not intended that all the terms in this Glossary be rigorously accurate or complete. Realistically, this is impossible. Depending on the circumstance, a particular term may have several meanings; this can never change. The primary purpose of this Glossary is to define the terms found in the Highway Drainage Guidelines and Model Drainage Manual in a manner that makes them easier to interpret and understand. A lesser purpose is to provide a compendium of terms that will be useful for both the novice as well as the more experienced hydraulics engineer. This Glossary may also help those who are unfamiliar with highway drainage design to become more understanding and appreciative of this complex science as well as facilitate communication between the highway hydraulics engineer and others. Where readily available, the source of a definition has been referenced. For clarity or format purposes, cited definitions may have some additional verbiage contained in double brackets [ ]. Conversely, three “dots” (...) are used to indicate where some parts of a cited definition were eliminated. Also, as might be expected, different sources were found to use different hyphenation and terminology practices for the same words. Insignificant changes in this regard were made to some cited references and elsewhere to gain uniformity for the terms contained in this Glossary: as an example, “groundwater” vice “ground-water” or “ground water,” and “cross section area” vice “cross-sectional area.” Cited definitions were taken primarily from two sources: W.B.
    [Show full text]
  • Modeling and Simulation of High-Speed Wake Flows
    Modeling and Simulation of High-Speed Wake Flows A DISSERTATION SUBMITTED TO THE FACULTY OF THE GRADUATE SCHOOL OF THE UNIVERSITY OF MINNESOTA BY Michael Daniel Barnhardt IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY Graham V. Candler, Adviser August 2009 c Michael Daniel Barnhardt August 2009 Acknowledgments The very existence of this dissertation is a testament to the support and en- couragement I’ve received from so many individuals. Foremost among these is my adviser, Professor Graham Candler, for motivating this work, and for his consider- able patience, enthusiasm, and guidance throughout the process. Similarly, I must thank Professor Ellen Longmire for allowing me to tinker around late nights in her lab as an undergraduate; without those experiences, I would’ve never been stimulated to attend graduate school in the first place. I owe a particularly large debt to Drs. Pramod Subbareddy, Michael Wright, and Ioannis Nompelis for never cutting me any slack when I did something stupid and always pushing me to think bigger and better. Our countless hours of discussions provided a great deal of insight into all aspects of CFD and buoyed me through the many difficult times when codes wouldn’t compile, simulations crashed, and everything generally seemed to be broken. I also have to thank Travis Drayna and all of my other friends and colleagues at the University of Minnesota and NASA Ames. Dr. Matt MacLean of CUBRC and Dr. Anita Sengupta at JPL provided much of the experimental results and were very helpful throughout the evolution of the project.
    [Show full text]
  • Computational Turbulent Incompressible Flow
    This is page i Printer: Opaque this Computational Turbulent Incompressible Flow Applied Mathematics: Body & Soul Vol 4 Johan Hoffman and Claes Johnson 24th February 2006 ii This is page iii Printer: Opaque this Contents I Overview 4 1 Main Objective 5 2 Mysteries and Secrets 7 2.1 Mysteries . 7 2.2 Secrets . 8 3 Turbulent flow and History of Aviation 13 3.1 Leonardo da Vinci, Newton and d'Alembert . 13 3.2 Cayley and Lilienthal . 14 3.3 Kutta, Zhukovsky and the Wright Brothers . 14 4 The Navier{Stokes and Euler Equations 19 4.1 The Navier{Stokes Equations . 19 4.2 What is Viscosity? . 20 4.3 The Euler Equations . 22 4.4 Friction Boundary Condition . 22 4.5 Euler Equations as Einstein's Ideal Model . 22 4.6 Euler and NS as Dynamical Systems . 23 5 Triumph and Failure of Mathematics 25 5.1 Triumph: Celestial Mechanics . 25 iv Contents 5.2 Failure: Potential Flow . 26 6 Laminar and Turbulent Flow 27 6.1 Reynolds . 27 6.2 Applications and Reynolds Numbers . 29 7 Computational Turbulence 33 7.1 Are Turbulent Flows Computable? . 33 7.2 Typical Outputs: Drag and Lift . 35 7.3 Approximate Weak Solutions: G2 . 35 7.4 G2 Error Control and Stability . 36 7.5 What about Mathematics of NS and Euler? . 36 7.6 When is a Flow Turbulent? . 37 7.7 G2 vs Physics . 37 7.8 Computability and Predictability . 38 7.9 G2 in Dolfin in FEniCS . 39 8 A First Study of Stability 41 8.1 The linearized Euler Equations .
    [Show full text]
  • Introduction to Turbulent Flow
    CBE 6333, R. Levicky 1 Introduction to Turbulent Flow Turbulent Flow. In turbulent flow, the velocity components and other variables (e.g. pressure, density - if the fluid is compressible, temperature - if the temperature is not uniform) at a point fluctuate with time in an apparently random fashion. In general, turbulent flow is time-dependent, rotational, and three dimensional – thus, methods such as developed for potential flow in handout 13 do not work. For instance, measurement of the velocity component v1 at some stationary point in the flow may produce a plot as shown in Figure 1. In Figure 1, the velocity can be regarded as consisting of an average value v1 indicated by the dashed line, plus a random fluctuation v1' v1(t) = v1 (t) + v1'( t) (1) Figure 1 Similarly, other variables may also fluctuate, for example p(t) = p (t) + p'( t) (2) ρ(t) = ρ (t) + ρ'( t) (3) The overscore denotes average values and the prime denotes fluctuations. Turbulence will always occur for sufficiently high Re numbers, regardless of the geometry of flow under consideration. The origin of turbulence rests in small perturbations imposed on the flow; for instance, by wall roughness, by small variations in fluid density, by mechanical vibrations, etc. At low Re numbers such disturbances are damped out by the fluid viscosity and the flow remains laminar, but at high Re (when convective momentum transport dominates over viscous forces) they can grow and propagate, giving rise to the chaotic phenomena perceived as turbulence. Turbulent flows can be very difficult to analyze. In this handout, some of the simplest concepts pertinent to turbulent flows are introduced.
    [Show full text]