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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 3. CHANNEL FLOW 37<br />

u 2 + = 〈u 2 〉<br />

U 2 τ<br />

v 2 + = 〈v 2 〉<br />

U 2 τ<br />

Sometimes the driving pressure gradient is nondimensionalised by<br />

<br />

P + x =<br />

<br />

∂〈P 〉<br />

∂x<br />

2<br />

(Uτ ) ρ<br />

δ<br />

(3.30)<br />

(3.31)<br />

(3.32)<br />

Note that 〈u 2 〉 and 〈v 2 〉 may be nondimensionalised as 〈u2 〉<br />

k<br />

also notable that the definitions of Reτ and y + give<br />

y + |y=δ = Reτ<br />

3.4 Steady <strong>Channel</strong> <strong>Flow</strong> Data<br />

and 〈v2 〉<br />

. It is<br />

k<br />

(3.33)<br />

Based on the wealth of experimental and DNS results available concerning<br />

the behaviour of steady channel flows, a set of empirical profiles have been<br />

developed <strong>to</strong> obtain estimates of U + , − 〈uv〉 + , k + , 〈u 2 〉 + , and 〈v 2 〉 + . <strong>The</strong>se<br />

results are compared <strong>to</strong> DNS and experimental data in the following sections.<br />

Much of the data were found in the AGARD Aerospace Database 1 . <strong>The</strong><br />

contribu<strong>to</strong>rs of specific data sets are cited in the graph legends 2 .<br />

1 Advisory Group for Aerospace Research and Development, France<br />

2 Another excellent source of experimental information may be found at<br />

http://www.efluids.com. Furthermore, at http://<strong>to</strong>rroja.dmt.vpm.es Dr. Javier Jimenez<br />

(School of Aeronautics, University of Madrid) has published full flow fields for channel<br />

flow at Reτ = 180 and Reτ = 550

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