Turbulent Shear Flows I 1979
DOI: 10.1007/978-3-642-46395-2_18
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The Calculation of Two-Dimensional Turbulent Recirculating Flows

Abstract: Numerical predictions are presented for seven different two-dimensional turbulent "elliptic" flows. The solution procedure, which is embodied in the TEACH computer program, is described and numerical tests reported. The calculated properties of the seven flows are compared with experimental results and demonstrate that the procedure, with a two-equation turbulence model, provides adequate precision for many engineering applications. The two-equation model is shown, however, to be deficient in detail.

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Cited by 78 publications
(52 citation statements)
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“…In order to obtain the finite difference forms of the gas field governing equations which are based on the Eulerian approach, the TEACH code [23], which had been used to model the spray combustion by Choi and Baek [24], is modified. Also, the well-known SIMPLE (semi-implicit method for pressure-linked equations) algorithm [25] is applied to solve these equations.…”
Section: Methodsmentioning
confidence: 99%
“…In order to obtain the finite difference forms of the gas field governing equations which are based on the Eulerian approach, the TEACH code [23], which had been used to model the spray combustion by Choi and Baek [24], is modified. Also, the well-known SIMPLE (semi-implicit method for pressure-linked equations) algorithm [25] is applied to solve these equations.…”
Section: Methodsmentioning
confidence: 99%
“…Consequently, the resultant velocity parallel to the wall in question and at a distance y 1 (where y + ≤30) from it corresponding to the first grid node was assumed to be represented by the law of the wall equations [14], i.e. :…”
Section: Mathematical Modelingmentioning
confidence: 99%
“…The set of governing equations for the parabolic method are conservation of mass, the axial Navier-Stokes equation ( 1 (.L ( r pu ) + _L ( r pv) ) = 0 r ax ar ( 1) Axial Momentum: terms appearing in these equations will be defined once the finite difference form of these equations has been developed.…”
Section: Differential Equationsmentioning
confidence: 99%
“…The source term necessary to modify the near wall turbulent kinetic energy equation follows (9) The calculations of this expression may be broken into and T is calculated from Equation 17 and u+ is calculated from …”
Section: Finite Difference Equationsmentioning
confidence: 99%
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