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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 5. RESULTS 74<br />

where y/δ = 0.2, the log law produces results for k + that are in phase with the<br />

results for 〈U〉 + . This is <strong>to</strong> be expected from the log law equations. Further<br />

from the wall, where the k-ε model equations are applied, the generated<br />

result is improved, but still offers little encouragement as <strong>to</strong> the applicability<br />

of the log law <strong>to</strong> this flow.<br />

Examining turbulent kinetic energy, k + in Figures 5.7, 5.8, 5.9 & 5.10, it<br />

appears that the subgrid k-ε treatment closely matches the low-Reynolds-<br />

number k-ε solution for y/δ ≤ 0.2, within the subgrid region. Outside of the<br />

subgrid region (Figures 5.9 & 5.10), the subgrid solution appears <strong>to</strong> capture<br />

the effects of variations in<br />

∂〈P 〉<br />

∂x<br />

slightly less effectively than the low-Reynolds-<br />

number counterpart. This suggests that the process of averaging the subgrid<br />

solution <strong>to</strong> be applied as a boundary condition <strong>to</strong> the main grid introduces<br />

some discernible measure of inaccuracy. <strong>The</strong> subgrid solution can therefore<br />

produce different results than a calculation that is continuous throughout the<br />

flow field (standard low-Reynolds-number treatment), even when the same<br />

turbulence model is used in each case.<br />

<strong>The</strong> k-ω solution produces and amplitude of oscillation of τw that more closely<br />

matches the DNS than that produced by the k-ε subgrid solution (Figure<br />

5.6). Correspondingly, the k-ω model produces fluctuations in bulk velocity<br />

that are also slightly improved (Figure 5.5). This is an indication of the<br />

applicability of the k-ω model <strong>to</strong> boundary layer flow. <strong>The</strong> k-ω model exhibits<br />

a less prominent peak in turbulent kinetic energy than is produced by the<br />

k-ε model (Figures 5.7, 5.8, 5.9 & 5.10). This may be compounded by the<br />

general tendency of the k-ω model <strong>to</strong> offer lower values of k, as observed in<br />

the steady flow results.

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