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Basics of Fluid Mechanics, 2014a

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8.7. EXAMPLES FOR DIFFERENTIAL EQUATION (NAVIER-STOKES) 263<br />

The pressure integral is<br />

∫<br />

(<br />

PdA=(P zd z − P z ) πr 2 = P z + ∂P )<br />

∂z dz − P z πr 2 = ∂P<br />

∂z dz π r2 (8.140)<br />

The last term is<br />

∫<br />

∫<br />

ρU z U rn dA = ρ<br />

(∫<br />

ρ U 2 z+dz dA<br />

z+dz<br />

U z U rn dA =<br />

∫ )<br />

− U 2 z dA<br />

z<br />

∫<br />

(<br />

= ρ<br />

2 2 Uz+dz − U ) z dA<br />

z<br />

(8.141)<br />

The term U z+dz 2 − U z 2 is zero because U z+dz = U z because mass conservation conservation<br />

for any element. Hence, the last term is<br />

∫<br />

ρU z U rn dA =0 (8.142)<br />

Substituting equation (8.139) and (8.140) into equation (8.138) results in<br />

μ dU z<br />

dr 2 ✚π ✁ r ✚dz = − ∂P<br />

∂z ✚dz ✚πr✄ 2 (8.143)<br />

Which shrinks to<br />

2 μ<br />

r<br />

dU z<br />

dr<br />

= −∂P ∂z<br />

(8.144)<br />

Equation (8.144) is a first order differential equation for which only one boundary<br />

condition is needed. The “no slip” condition is assumed<br />

U z (r = R) =0 (8.145)<br />

Where R is the outer radius <strong>of</strong> pipe or cylinder. Integrating equation (8.144) results in<br />

U z = − 1 ∂P<br />

μ ∂z r2 + c 1 (8.146)<br />

It can be noticed that asymmetrical element 25 was eliminated due to the smart short<br />

cut. The integration constant obtained via the application <strong>of</strong> the boundary condition<br />

which is<br />

c 1 = − 1 ∂P<br />

μ ∂z R2 (8.147)<br />

The solution is<br />

U z = 1 (<br />

∂P<br />

( r<br />

) ) 2<br />

μ ∂z R2 1 −<br />

(8.148)<br />

R<br />

While the above analysis provides a solution, it has several deficiencies which include the<br />

ability to incorporate different boundary conditions such as flow between concentering<br />

cylinders.<br />

25 Asymmetrical element or function is −f(x) =f(−x)

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