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Basics of Fluid Mechanics, 2014a

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96 CHAPTER 4. FLUIDS STATICS<br />

Calculation <strong>of</strong><br />

the correction<br />

factor<br />

dA<br />

ω<br />

Rotation<br />

center<br />

S<br />

constant pressure line<br />

L<br />

xL<br />

Fig. -4.17. Schematic angular angle to explain example 4.11.<br />

It is first assumed that the height is uniform at the tube (see for the open question on<br />

this assumption). The pressure at the interface at the two sides <strong>of</strong> the tube is same.<br />

Thus, equation (4.89) represents the pressure line. Taking the “left” wing <strong>of</strong> U tube<br />

change in z direction<br />

{ }} {<br />

z l − z 0 =<br />

The same can be said for the other side<br />

change in r direction<br />

{ }} {<br />

ω 2 L 2<br />

2 g<br />

z r − z 0 = ω2 x 2 L 2<br />

2 g<br />

Thus subtracting the two equations above from each each other results in<br />

(<br />

z r − z l = Lω2 1 − x 2)<br />

2 g<br />

It can be noticed that this kind equipment can be used to find the gravity.<br />

End Solution<br />

Example 4.12:<br />

Assume that the diameter <strong>of</strong> the U tube is R t . What will be the correction factor if the<br />

curvature in the liquid in the tube is taken in to account. How would you suggest to<br />

define the height in the tube?<br />

Solution<br />

In Figure 4.17 shows the infinitesimal area used in these calculations. The distance <strong>of</strong><br />

the infinitesimal area from the rotation center is ?. The height <strong>of</strong> the infinitesimal area<br />

is ?. Notice that the curvature in the two sides are different from each other. The<br />

volume above the lower point is ? which is only a function <strong>of</strong> the geometry.<br />

End Solution<br />

Example 4.13:<br />

In the U tube in example 4.11 is rotating with upper part height <strong>of</strong> l. At what rotating

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