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Chapter 9 Viscous flow

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6 CHAPTER 9. VISCOUS FLOW<br />

The velocity field in the momentum equation can be separated into two<br />

parties, a ‘homogeneous solution’ which satisfies<br />

and a particular solution which satisfies<br />

∂ 2 i u (h)<br />

i = 0 (9.12)<br />

µ∂ 2 i u(p) i = ∂ i p (9.13)<br />

The particular solution is any one solution to the equation 9.13. One solution<br />

which satisfies equation 9.13 is<br />

u (p)<br />

i = 1<br />

2µ px i (9.14)<br />

This solution can be verified as follows. If we take the gradient of the particular<br />

solution 9.14, we get<br />

∂ j u (p)<br />

i = 1<br />

2µ (x i∂ j p + pδ ij ) (9.15)<br />

Upon taking the divergence of the above equation, we get<br />

∂j 2 u(p) i = 1<br />

2µ (2δ ij∂ j p + x i ∂j 2 p)<br />

= 1 µ ∂ ip (9.16)<br />

Therefore, the velocity fields can be obtained by solving the Laplace equation<br />

for the pressure and the homogeneous part of the velocity fields, and using<br />

equation 9.16 to obtain the particular part of the velocity field.<br />

We have already studied the solution for the Laplace equation,<br />

∇ 2 φ = 0 (9.17)<br />

which are obtained using separation of variables. In the present chapter, we<br />

derive the same solutions using the more convenient indicial notation. The<br />

fundamental solution for the Laplace equation in three dimensions, correct<br />

to within a multiplicative constant (which is determined from the boundary<br />

conditions, is<br />

Φ (0) = 1 r<br />

(9.18)

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