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Basics of Fluid Mechanics, 2014a

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344 CHAPTER 10. POTENTIAL FLOW<br />

The volumetric flow rate (two dimensional)<br />

˙Q denotes the flow rate out<br />

or in to control volume into the source or<br />

sink. The flow rate is shown in Figure 10.7<br />

is constant for every potential line. The<br />

flow rate can be determined by<br />

˙Q =2πrU r (10.81)<br />

Where ˙Q is the volumetric flow rate, r<br />

is distance from the origin and U r is the<br />

velocity pointing out or into the origin<br />

depending whether origin has source or<br />

sink. The relationship between the potential<br />

function to velocity dictates that<br />

9.0<br />

7.0<br />

5.0<br />

3.0<br />

1.0<br />

-9.0 -7.0 -5.0 -3.0 -1.0 1.0 3.0 5.0 7.0 9.0<br />

-2.0<br />

-4.0<br />

-6.0<br />

-8.0<br />

ψ = const<br />

ψ =0<br />

φ = const<br />

Fig. -10.7. Streamlines and Potential lines due<br />

to Source or sink.<br />

∇φ = U = U ̂r =<br />

˙Q<br />

(10.82)<br />

2 πr̂r<br />

Explicitly writing the gradient in cylindrical coordinate results as<br />

∂φ<br />

∂r̂r + 1 ∂φ<br />

r ∂θ ̂θ + ∂φ<br />

∂z ẑ =<br />

˙Q<br />

2 πr̂r +0̂θ +0ẑ (10.83)<br />

Equation (10.83) the gradient components must satisfy the following<br />

The integration <strong>of</strong> equation results in<br />

∂φ<br />

∂r =<br />

˙Q<br />

2 πr̂r<br />

∂φ<br />

∂z = ∂φ<br />

(10.84)<br />

∂θ =0<br />

φ − φ 0 =<br />

˙Q<br />

2 πr ln r (10.85)<br />

r 0<br />

where r 0 is the radius at a known point and φ 0 is the potential at that point. The stream<br />

function can be obtained by similar equations that were used or Cartesian coordinates.<br />

In the same fashion it can be written that<br />

dψ = U·ŝdl (10.86)<br />

Where in this case dl = rdθ (the shortest distance between two adjoining stream lines<br />

is perpendicular to both lines) and hence equation (10.87) is<br />

dψ = U· rdθ̂r̂r̂r =<br />

˙Q ˙Q<br />

rdθ=<br />

2 πr 2 π<br />

dθ (10.87)

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