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The UMIST-N Near-Wall Treatment Applied to Periodic Channel Flow

The UMIST-N Near-Wall Treatment Applied to Periodic Channel Flow

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CHAPTER 1. INTRODUCTION & LITERATURE SURVEY 7<br />

work of Kolmogorov [31] and Saffman [65], Wilcox [89] proposed the most<br />

well-known k-ω model. <strong>The</strong> model does not require the same damping terms<br />

employed by the standard k-ε model in order <strong>to</strong> be effective in the near-wall<br />

region, but boundary conditions are more difficult <strong>to</strong> apply. <strong>The</strong> principal<br />

difficulty associated with the k-ω model is in specifying a value for ω in free-<br />

stream turbulence [40]. Speziale et al. [76], Menter [41], Peng et al. [52],<br />

and Wilcox [90] have proposed modifications <strong>to</strong> the k-ω that further improve<br />

its performance at the cost of adding much the same degree of complexity<br />

found in the standard k-ε model.<br />

<strong>The</strong> SST 2 model of Menter [42] may be thought of as a hybrid k-ε / k-ω<br />

approach. It employes a k-ω model near solid boundaries and a k-ε model<br />

elsewhere. <strong>The</strong> SST model is appealing because the principal strength of<br />

the k-ω model is its simplicity and relative accuracy in the near-wall region,<br />

while the k-ε model is generally more effective in free-stream flow. <strong>The</strong> SST is<br />

implemented by the use of a blending function <strong>to</strong> provide a smooth transition<br />

between the two models.<br />

1.3 <strong>Wall</strong> Functions & the Subgrid Approach<br />

<strong>Near</strong> solid boundaries, the gradients of turbulence quantities become large.<br />

Numerically, this means that greater s<strong>to</strong>rage and computational demands are<br />

placed on a CFD code that performs calculations in the near-wall region. To<br />

avoid this, wall functions are often employed. A wall function is a solution<br />

method that provides a means of characterising turbulence at some point,<br />

2 Shear Stress Transport

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