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  • 1
    Monograph available for loan
    Monograph available for loan
    Dordrecht [u.a.] :Kluwer
    Associated volumes
    Call number: AWI A13-02-0060
    In: Fluid mechanics and its applications
    Description / Table of Contents: Table of Contents: Preface and Acknowledgments. - 1 Introductory comments and summary. - 1.1 Introduction. - 1.2 Summary of the chapters. - 1.3 Conclusions. - 2 Finite differences. - 2.1 Introduction. - 2.2 Difference operators. - 2.2.1 Space discretization. - 2.2.2 Non-uniform grids. - 2.2.3 Coordinate transformations. - 2.2.3a Two walls clustering. - 2.2.3b Uniform in the center, stretched in the far field. - 2.2.3c Clustered in the center. - 2.2.3d Clustered around two inner regions. - 2.2.3e Clustered near two walls and at the center. - 2.2.3f Clustered in one region and stretched elsewhere. - 2.2.4 Non-uniform grids boundary conditions. - 2.3 Parabolic equations intime. - 2.3.1 Crank-Nicholson implicit scheme. - 2.3.2 Adams-Bashfort explicit. - 2.3.3 Low storage third-order Runge-Kutta Explicit. - 2.3.4 Hybrid third-order Runge-Kutta/Crank-Nicholson. - 2.3.5 Third order Runge-Kutta vs Adams-Bashfort. - 2.4. FFT for elliptic partial differential equations. - 2.4.1 Solution by FFT. - 2.4.2 Two periodic directions. - 2.4.3 sinFFT. - 2.4.4 cosFFT centered. - 2.4.5 cosFFT "staggered". - 2.5 Multigrid methods for elliptic partial differential equations. - 2.5.1 Multigrid method. - 2.6 Conclusions. - 3 The Burgers equation. - 3.1 Physical considerations. - 3.2 Spatial discretization. - 3.3 Time discretization. - 3.4 Results. - 3.5 Conclusions. - 4 Two-dimensional flows in Cartesian coordinates. - 4.1. Introduction. - 4.2 The equations in vorticity-streamfunction formulation. - 4.3 Vorticity boundary conditions. - 4.3a Periodicity. - 4.3b Free-slip. - 4.3c No-slip. - 4.3d Outlet. - 4.4 Streamfunction boundary conditions. - 4.5 Physical aspects of nonlinear terms. - 4.6 Arakawa's scheme. - 4.7 Nonlinear terms in primitive variables. - 4.8. Viscous terms and factorization. - 4.9 Boundary conditions. - 4.10 Test of [Omega, Psi] formulation. - 4.11 Code PSOMGBC. - 4.11a Input data. - 4.11b Initial conditions. - 4.11b.a Lamb dipole. - 4.11b.b Stern dipole. - 4.11b.c Isolated vortex. - 4.11b.d Monopole in a [Beta] plane. - 4.11b.e Flow near a coast with topography slopes. - 4.11b.f Time developing mixing layer. - 4.11b.g Space developing mixing layer. - 4.12 Results by the code PSOMGBC. - 4.12.1 General suggestion. - 4.12.2 Flow phenomena simulations. - 4.12.2a Lamb dipoles. - 4.12.2b Modons. - 4.12.2c Tripoles. - 4.12.2d Monopols in a [Beta] plane. - 4.12.2e Flow over topographic slopes. - 4.12.2f Time developing mixing layers. - 4.12.2g Roll-up. - 4.12.2h The pairing. - 4.12.2i Arakawa scheme effects. - 4.12.2j Space developing mixing layers. - 4.13 Conclusions. - 5 Two-dimensional flows in general curvilinear coordinates. - 5.1 Introduction. - 5.2 Equations. - 5.3 Laplacian discretization. - 5.4 Nonlinear terms discretization. - 5.5 Boundary conditions. - 5.6 Time discretization. - 5.7Code PSOMCUR. - 5.8 Results. - 5.8a Inviscid dipole moving close to a bump. - 5.8b Dipole impinging a semicircular cavity. - 5.8c Stream around a Gaussian hill. - 5.9 Conclusions. - 6 Two-dimensional turbulence. - 6.1. Introduction. - 6.2 Arakawa fourth order scheme. - 6.3 Initial conditions. - 6.4 Code TURB2D. - 6.5 Results. - 6.5.1 Resolution check. - 6.5.2 Global conservation properties. - 6.6 Conclusions. - 7 Axisymmetric flows. - 7.1 Introduction. - 7.2 Equations for the vorticity formulation. - 7.3 Results. - 7.3a Vortex ring formation. - 7.3b Vortex ring in the presence of solid body rotation. - 7.3c Vortex rings impacting free-slip walls. - 7.3d Vortex rings impacting no-slip walls. - 7.3e Space developing coaxial jet. - 7.4 Conclusions. - 8 Three-dimensional flows with three periodic directions. - 8.1 Introduction. - 8.2 Governing equations. - 8.3 Space and time discretization. - 8.4 Discretization of the non-linear terms. - 8.5 Fractional step. - 8.6 Factorization in the [Ypsilon]i equations. - 8.7 Solution of the Poisson equation for [Phi]. - 8.8 Initial conditions. - 8.8.1 Isotropic turbulence. - 8.8.2 Lamb dipole stability. - 8.9 Numerical checks of the code ISO. - 8.10 Definition of turbulent quantities. - 8.11 Isotropic turbulence with and without rotation. - 8.11a Isotropic turbulence. - 8.11b Isotropic turbulence subjected to uniform rotation. - 8.12 Physics of turbulence from data. - 8.12.a Correlation tensor. - 8.12.b Probability Density Functions. - 8.12.b.1 PDF of velocity and vorticity components. - 8.12.b.2 PDF of pressure field. - 8.12.b.3 PDF of angle between velocity and vorticity vectors. - 8.12.b.4 Velocity structure functions. - 8.13 Stability of the Lamb dipole to three dimensional disturbances. - 8.14 Conclusions. - 9 Flows with walls in Cartesian coordinates. - 9.1 Introduction. - 9.2 Adimensionalization. - 9.3 Space and time discretization. - 9.4 Initial conditions. - 9.5 Wall boundaries for turbulence control. - 9.6 Definition of turbulent quantities. - 9.7 Check of the code CHADS. - 9.8 Wall-boundary conditions effects. - 9.9 Analysis of the data. - 9.9a Velocity statistics. - 9.9b Vorticity statistics. - 9.9c Production and dissipation rate. - 9.9d Velocity vorticity tensor. - 9.9e Velocity vorticity spectra. - 9.9f Velocity and vorticity cospectra. - 9.9g Velocity and vorticity two-point correlations. - 9.9h Joint PDF of velocity and vorticity correlations in one point. - 9.9i Vortex stretching. - 9.9j Budget in the one-point closure equations. - 9.10 Conclusions. - 10 Flows in cylindrical coordinates with one wall. - 10.1 Introduction. - 10.2 Governing equations. - 10.3. Numerical method. - 10.4. Treatment of the axis. - 10.5 Code informations. - 10.5a Calculation of qi (first step). - 10.5b Calculation of qi n+1 (second step). - 10.5c Initial conditions. - 10.6 Results. - 10.6a Check of axis accuracy. - 10.6b Check of energy conservation. - 10.6c Turbulent non-rotating pipe, coarse solution. - 10.6b Turbulent rotating pipe, coarse solution. - 10.7 Conclusions. - 11 Flows in cylindrical coordinates with two walls. - 11.1 Introduction. - 11.2 Governing equations and numerical model. - 11.3 Code general informations. - 11.3a Description of the file tr3dnuma.f. - 11.3b Description of the file fr3dnuge.f. - 11.3c Description of the file tr3dnucoJ. - 11.3d Description of the file tr3dnuintr.f. - 11.3e Description of the file tr3dnuinri.f. - 11.3f Description of the file tr3dnuhnJ. - 11.3g Description of the file tr3dnutnJ. - 11.3h Description of the file tr3dnutr.f. - 11.3i Description of the file tr3dnutu.f. - 11.3j Description of the file tr3dnuioJ. - 11.4 Results. - 11.4a Three-dimensional tripole formation. - 11.4b Three-dimensional impact of a vortex ring on a wall. - 11.5 Conclusions. - 12 Large eddy simulations. - 12.1. Introduction. - 12.2. Filtering. - 12.3. Equations. - 12.4. Subgrid models. - 12.4a Smagorinsky model for the residual stress. - 12.4b Structure function model. - 12.4c Dynamic subgrid model. - 12.4d Similarity scale models. - 12.5 Equations for density-Related problems. - 12.6 Subgrid model for the rmal flows. - 12.7 Code informations. - 12.7a Description of the file isolesma.f. - 2.7b Description of the file isolesnn.f. - 12.7c Description of the file isoleshn.f. - 12.7d Description of the file isolestn.f. - 12.7e Description of the file isolestnsi.f. - 12.7f Description of the file isolesintu.f . - 12.7g Description of the file isolesinsi.f. - 12.7h Description of the file isolesph.f. - 12.7i Description of the file isolessp.f. - 12.7j Description of the file isolesst.f. - 12.7k Description of the file isolestr.f. - 12.71 Description of the file isolesio.f. - 12.7m Description of the file isolesiosi.f. - 12.7n Subgrid-models. - 12.8 Results. - 12.8a Grid turbulence at intermediate R [Lambda]. - 12.8b Isotropic turbulence at high R [Lambda]. - 12.8c Isotropic turbulence with a passive scalar. - 12.8d Buoyancy-generated turbulence. - 12.8e Turbulence with buoyancy and stratification. - 12.9 Conclusions. - 13 Large eddy simulations of wall-bounded flows. - 13.1. Introduction. - 13.2. Equations. - 13.3. Results. - 13.3.a Results at low Reynolds number. - 13.3.a Results at high Reynolds numbers. - 13.4 Conclusions. - References. - Diskette information. - Plates section.
    Description / Table of Contents: This book deals with the simulation of the incompressible Navier-Stokes equations for laminar and turbulent flows. The book is limited to explaining and employing the finite difference method. This book furnishes a large number of source codes which permit to play with the Navier-Stokes equations and to understand the complex physics related to fluid mechanics. Numerical simulations are useful tools to understand the complexity of the flows, which often is difficult to derive from laboratory experiments. This book, then, can be very useful to scholars doing laboratory experiments, since they often do not have extra time to study the large variety of numerical methods; furthermore they cannot spend more time in transfering one of the methods into a computer language. By means of numerical simulations, for example, insights into the vorticity field can be obtained which are difficult to obtain by measurements. This book can be used by graduate as well as undergraduate students while reading books on theoretical fluid mechanics; it teaches how to simulate the dynamics of flow fields on personal computers. This will provide a better way of understanding the theory. Two chapters on Large Eddy Simulations (LES) habe been included since it is a methodology that in the near future will allow having more universal turbulence models for practical applications. The direct simulation of the Navier-Stokes equations (DNS) is simple by finite-differences, that are satisfactory to reproduce the dynamics of turbulent flows. A large part of the book is devoted to study homogeneous and wall turbulent flows. In the second chapter the elementary concept of finite difference is given to solve parabolic and elliptical partial differential equations. In successive chapters the 1D, 2D, and 3D Navier-Stokes equations are solved in Cartesian and cylindrical coordinates. Finally, Large Eddy Simulations are performed to check the importance of the subgrid scale models. Results for turbulent and laminar flows are discussed with particular emphasis on vortex dynamics. This volume will be of interest to graduate students and researchers wanting to compare experiments and numerical simulations, and to workers in the mechanical and aeronautic industries.
    Type of Medium: Monograph available for loan
    Pages: XII, 356 S. : Ill. ; 25 cm. + Diskette (3,5")
    Edition: Repr. 2001
    ISBN: 0792360958
    Series Statement: Fluid mechanics and its applications 55
    Branch Library: AWI Library
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  • 2
    Electronic Resource
    Electronic Resource
    New York, NY : American Institute of Physics (AIP)
    Physics of Fluids 2 (1990), S. 1429-1436 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: Accurate numerical simulations of vortex dipoles impinging on flat boundaries have revealed interesting new features. In the case of free-slip boundaries the dipole does not rebound from the wall. In the case of nonslip walls rebounding occurs and complex interactions of secondary and tertiary vortices appear. The numerical simulation of the first dipole rebound from the wall agrees with experimental visualizations. Numerical experiments extending in time beyond the real experiments show multiple rebounding. Each rebound is associated with the detachment of a secondary vorticity layer from the wall, these layers merge, and at a value of Reynolds number Re=1600, form a new dipole. This dipole has sufficient circulation to induce on itself a motion in the opposite direction to the motion of the initial dipole.
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    [S.l.] : American Institute of Physics (AIP)
    Physics of Fluids 6 (1994), S. 634-641 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: The formation of streaky velocity structures in the near wall region of turbulent boundary layers is studied through a simplified two-dimensional computational model in the plane normal to the average velocity. It is shown that the redistribution of the longitudinal velocity by streamwise vortices produces features very similar to those observed in the experiments, and that compact streamwise vortices form naturally from more general vorticity distributions. It is also shown, both numerically and analytically, that one effect of the formation of the streaks is to increase the average wall friction, and it is suggested that this effect is responsible for the higher friction in turbulent boundary layers, as opposed to laminar ones. An approximate quantitative analysis of the process supports this assumption.
    Type of Medium: Electronic Resource
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  • 4
    Electronic Resource
    Electronic Resource
    New York, NY : American Institute of Physics (AIP)
    Physics of Fluids 3 (1991), S. 1463-1463 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: The interaction of vortices with fixed boundaries is an important problem in many areas of practical interest. During the approach of the vortices to the wall, vorticity is created at the wall, and then mixing and stirring of primary and secondary vorticity lead to different scenarios that depend on the Re number. This problem is relevant to bursting in turbulent boundary layers, which is responsible for turbulence production. In the near-wall region of turbulent flows, vortex stretching plays a fundamental role. As a prelude to attempting the solution by direct simulation of 3-D Navier–Stokes equations, it is convenient to describe the mechanism associated with 2-D or axisymmetric flows. In the present study, axisymmetric vortex rings and vortex dipoles approaching a nonslip flat wall have been considered. In both cases, experimental results based on flow visualization are available.1,2 The purpose of the present paper is to do a numerical simulation with the same conditions used in the real experiments and follow the flow evolution for a much longer time than has been possible in such experiments. Both for axisymmetric and 2-D cases the numerical simulation shows, as revealed by the experiments, that, at the initial stage, very thin layers of vorticity of sign opposite to that of the primary vortex are generated at the wall.This mechanism is almost independent of Re. This thin and intense layer immediately becomes unstable and rolls up creating a secondary vortex. This vortex interacts with the primary vortex and different flow structures are generated, depending on Re. The location where these structures form depends, in large measure, on whether vortex stretching is present or not. Particularly relevant to the bursting phenomenon is the case at intermediate Re (e.g., Re=1600). Here, a new dipole is created near the wall after multiple rebounding and pairing of secondary vortices. This new structure has sufficient strength to move itself away from the wall. We conclude that mixing and stirring of vorticity are the relevant mechanisms influencing the whole process in a two-dimensional simulation. This ejection of a new structure was previously noticed in the interaction of vortex rings with a wall. From flow visualization, Walker et al., at Re=Γ/ν〉3500, observed the occurrence of azimuthal instabilities and, immediately after that, they noticed a new vortex ring was rapidly ejected away from the wall.2 From these observations, those authors argued that the ejection was due to the azimuthal instabilities. In the present paper, axisymmetric calculations have been done in the same range of numbers used in the experiment of Walker et al.2 From the time evolution of the vorticity distribution, we argue that vortex pairing is the main mechanism that contributes to the generation of the new ring rather than azimuthal instabilities. The numerical simulations clearly show that this new ring is created above the primary ring and not at its interior.
    Type of Medium: Electronic Resource
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  • 5
    Publication Date: 1994-02-01
    Print ISSN: 1070-6631
    Electronic ISSN: 1089-7666
    Topics: Physics
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  • 6
    Publication Date: 2018-04-01
    Print ISSN: 1742-6588
    Electronic ISSN: 1742-6596
    Topics: Physics
    Published by Institute of Physics
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  • 7
    Publication Date: 2011-03-11
    Print ISSN: 1386-6184
    Electronic ISSN: 1573-1987
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Published by Springer
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  • 8
    Publication Date: 2011-01-13
    Print ISSN: 1386-6184
    Electronic ISSN: 1573-1987
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Published by Springer
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  • 9
    Publication Date: 2006-08-12
    Print ISSN: 1386-6184
    Electronic ISSN: 1573-1987
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Published by Springer
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  • 10
    Publication Date: 2011-04-01
    Description: Volaschioite, ideally Fe3+ 4(SO4)O2(OH)6{middle dot}2H2O, occurs in a small magnetite-pyrite orebody near Fornovolasco, in the Apuan Alps, Tuscany, Italy. The new mineral species is associated with pyrite and iron oxyhydroxides. In the same occurrence, other iron sulfates were identified, including alum-(K), "copiapite", fibroferrite, halotrichite, melanterite, romerite, and voltaite. Volaschioite occurs as radial aggregates of bladed crystals, up to 100 {micro}m in length and less than 5 {micro}m across. The color is yellowish orange with an orange streak; the luster is vitreous to resinous. The mineral is transparent and strongly pleochroic. Electron-microprobe analyses lead to the empirical formula Fe4.16(SO4)0.92O2.32(OH)6{middle dot}2H2O; the calculated density is 3.03 g/cm3. Volaschioite is monoclinic, with a 16.068(4), b 3.058(1), c 10.929(2) A, {beta} 93.82(3){degrees}, V 535.8(2) A3, Z = 2, space group C2/m. The strongest three X-ray powder-diffraction lines [d in A(I)(hkl)] are: 8.03(100)(200), 4.37(24)(202), 3.989(22)(400). The single-crystal X-ray diffraction pattern shows the presence of additional very weak and streaked reflections indicating a doubling of the b parameter. The average structure of volaschioite is composed of ribbons of edge-sharing Fe-centered octahedra running along b, linked together by corner-sharing to form corrugated layers, decorated on both sides by sulfate groups. Additional H2O molecules are located between the layers. Volaschioite is the product of pyrite alteration in an oxidizing environment. The name of this new species refers to the ancient name of the type locality, Forno de Volaschio. This mineral and its name have been approved by the IMA-CNMNC (IMA2010-005).
    Print ISSN: 0008-4476
    Topics: Geosciences
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