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Basics of Fluid Mechanics, 2014a

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260 CHAPTER 8. DIFFERENTIAL ANALYSIS<br />

y<br />

U l<br />

dy<br />

z<br />

x<br />

flow direction<br />

Fig. -8.16. Flow between two plates, top plate is moving at speed <strong>of</strong> U l to the right (as<br />

positive). The control volume shown in darker colors.<br />

length is given as ΔP 23 . The upper surface is moving in velocity, U l (The right side is<br />

defined as positive).<br />

Solution<br />

In this example, the mass conservation yields<br />

=0<br />

{ ∫}} { ∫<br />

d<br />

ρdV = −<br />

dt<br />

cv<br />

cv<br />

ρU rn dA =0 (8.126)<br />

The momentum is not accumulated (steady state and constant density). Further because<br />

no change <strong>of</strong> the momentum thus<br />

∫<br />

ρU x U rn dA =0 (8.127)<br />

A<br />

Thus, the flow in and the flow out are equal. It can concluded that the velocity<br />

in and out are the same (for constant density). The momentum conservation leads<br />

∫ ∫<br />

− PdA+ τ xy dA =0 (8.128)<br />

cv<br />

The reaction <strong>of</strong> the shear stress on the lower surface <strong>of</strong> control volume based on Newtonian<br />

fluid is<br />

τ xy = −μ dU<br />

(8.129)<br />

dy<br />

On the upper surface is different by Taylor explanation as<br />

cv<br />

⎛<br />

∼ =0<br />

⎞<br />

{ }} {<br />

τ xy = μ ⎜<br />

dU<br />

⎝ dy + d2 U<br />

dy 2 dy + d 3 U<br />

dy 3 dy2 + ··· ⎟<br />

⎠ (8.130)<br />

23 The difference is measured at the bottom point <strong>of</strong> the plate.

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