Vijay K. Garg's Applied Computational Fluid Dynamics (Mechanical Engineering PDF

By Vijay K. Garg

ISBN-10: 0824701658

ISBN-13: 9780824701659

Describes the newest options and real-life purposes of computational fluid dynamics (CFD) and warmth move in aeronautics, fabrics processing and production, digital cooling, and environmental regulate. comprises new fabric from skilled researchers within the box. entire with distinct equations for fluid circulate and warmth move.

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Extra resources for Applied Computational Fluid Dynamics (Mechanical Engineering Series) (Dekker Mechanical Engineering)

Example text

5 Time Integration . . . . . . . . . . . 36 37 38 . 41 . 42 . 44 . 48 . 49 . 50 . 51 . 52 . 53 . 54 . 56 . 56 . 59 . 61 . 64 . 65 . 1 Garg Nomenclature . . . . . . . . . . . 70 References 71 . . . . . . . . . . . INTRODUCTION We notice from Chapter 1 that the equations governing fluid flow and heat transfer are complex partial differential equations for which no analytical solution can be found except in rather simple situations. For many practical problems, in general, obtaining a numerical solution to the Navier-Stokes equations is the only possibility, short of actual experimentation.

For elliptic equations, information at a point P in the x-y plane influences all other regions of the domain. Therefore, the solution at point P must be carried out simultaneously with the solution at all other points in the domain. This is in stark contrast to the ‘marching’ solutions germane to parabolic and hyperbolic equations. For inciscid compressible flows, the system of equations is always hyperbolic- if the motion is unsteady, no matter whether the flow is locally subsonic or supersonic.

11 j which is first-order accurate. 12) through the three points 1, 2, and 3 in Fig. 2. 13) Using a Taylor series expansion about point 1, it can be shown that Eq. 13) is second-order accurate. 14) Both Eqs. 14) are called one-sided di$erences, since they express a derivative at a point in terms of dependent variables on only one side of the point. Many other one-sided differences can be formed, with higher degrees of accuracy, using additional grid points (Hyman and Larrouturou, 1982). 3 Solution of Finite Difference Equations---Some Cons ider at ions As stated earlier, the FDM replaces the partial derivatives in the governing equations by the difference quotients, leading to a system of algebraic equations for the dependent variable(s) at each grid point.

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Applied Computational Fluid Dynamics (Mechanical Engineering Series) (Dekker Mechanical Engineering) by Vijay K. Garg

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