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7.9 Some Typical Model Studies 369<br />

SOLUTION<br />

The width, w m , of the model spillway is obtained from the length<br />

scale, l / , so that<br />

Therefore,<br />

(Ans)<br />

Of course, all other geometric features 1including surface roughness2<br />

of the spillway must be scaled in accordance with the same<br />

length scale.<br />

With the neglect of surface tension and viscosity, Eq. 7.24 indicates<br />

that dynamic similarity will be achieved if the Froude<br />

numbers are equal between model and prototype. Thus,<br />

and for g m g<br />

Since the flowrate is given by Q VA, where A is an appropriate<br />

cross-sectional area, it follows that<br />

where we have made use of the relationship A mA 1/ m/2 2 . For<br />

l and Q 125 m 3 / 1<br />

s<br />

15<br />

Q m<br />

Q V m<br />

VA<br />

w m<br />

w l / 1<br />

15<br />

w m 20 m<br />

15 1.33 m<br />

V m<br />

2g m / m<br />

<br />

V m<br />

V / m<br />

B /<br />

A m<br />

1l / 2 5 2<br />

/<br />

2<br />

m<br />

B / a/ m<br />

/ b<br />

Q m 1 1<br />

152 5 2 1125 m 3 s2 0.143 m 3 s<br />

(Ans)<br />

The time scale can be obtained from the velocity scale, since<br />

the velocity is distance divided by time 1V /t2, and therefore<br />

V<br />

/ t m<br />

V m t / m<br />

V<br />

2g/<br />

or<br />

t m<br />

t<br />

V / m<br />

V m / / m<br />

B / 2l /<br />

This result indicates that time intervals in the model will be<br />

smaller than the corresponding intervals in the prototype if<br />

l For l / 1 / 6 1.<br />

15 and a prototype time interval of 24 hr<br />

t m 2 1 15 124 hr2 6.20 hr (Ans)<br />

COMMENT As indicated by the above analysis, the time<br />

scale varies directly as the square root of the length scale. Thus,<br />

as shown in Fig. E7.8b, the model time interval, t m , corresponding<br />

to a 24-hr prototype time interval can be varied by changing<br />

the length scale, l / . The ability to scale times may be very useful,<br />

since it is possible to “speed up” events in the model which<br />

may occur over a relatively long time in the prototype. There is<br />

of course a practical limit to how small the length scale (and the<br />

corresponding time scale) can become. For example, if the<br />

length scale is too small then surface tension effects may<br />

become important in the model whereas they are not in the prototype.<br />

In such a case the present model design, based simply<br />

on Froude number similarity, would not be adequate.<br />

t m , hr<br />

20<br />

16<br />

12<br />

8<br />

4<br />

(1/15, 6.20 hr)<br />

0<br />

0 0.1 0.2<br />

m ___<br />

<br />

0.3 0.4 0.5<br />

F I G U R E E7.8b<br />

V7.20 Testing of<br />

large yacht mode<br />

There are, unfortunately, problems involving flow with a free surface in which viscous, inertial,<br />

and gravitational forces are all important. The drag on a ship as it moves through water is<br />

due to the viscous shearing stresses that develop along its hull, as well as a pressure-induced component<br />

of drag caused by both the shape of the hull and wave action. The shear drag is a function<br />

of the Reynolds number, whereas the pressure drag is a function of the Froude number. Since both<br />

Reynolds number and Froude number similarity cannot be simultaneously achieved by using water<br />

as the model <strong>fluid</strong> 1which is the only practical <strong>fluid</strong> for ship models2, some technique other than<br />

a straightforward model test must be employed. One common approach is to measure the total drag<br />

on a small, geometrically similar model as it is towed through a model basin at Froude numbers<br />

matching those of the prototype. The shear drag on the model is calculated using analytical techniques<br />

of the type described in Chapter 9. This calculated value is then subtracted from the total<br />

drag to obtain pressure drag, and using Froude number scaling the pressure drag on the prototype<br />

can then be predicted. The experimentally determined value can then be combined with a calculated<br />

value of the shear drag 1again using analytical techniques2 to provide the desired total drag

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