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Introduction to Acoustics

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Static efficiency normalized <strong>to</strong> its maximum value<br />

1.00<br />

0.80<br />

0.60<br />

0.40<br />

0.20<br />

0<br />

0<br />

0.020<br />

0.040<br />

0.060 0.080 0.100<br />

Volume flow rate (m 3 /s)<br />

Fig. 23.16 Illustration of air-moving device static efficiency<br />

for a constant input power<br />

large devices. In the design of small ventilating systems,<br />

the system resistance is often not known accurately, and<br />

optimal design may be difficult <strong>to</strong> achieve. However,<br />

an operating point <strong>to</strong> the left of the point of maximum<br />

static efficiency is usually undesirable, both from the<br />

viewpoint of flow instability and increased noise.<br />

The choice of a type of air-moving device is usually<br />

dictated by the desired specific speed Ns defined as<br />

Ns = NQ1/2<br />

P3/4 , (23.36)<br />

where N is the rotational speed of the air moving device,<br />

and P and Q are defined above. Axial flow devices are<br />

generally used at low pressures and high-volume flow<br />

rates (high specific speed), and centrifugal devices are<br />

usually used at relatively high pressures and low-volume<br />

flow rates (low specific speed).<br />

For noise radiation from large air-moving devices,<br />

it is often useful <strong>to</strong> use a sound law first proposed by<br />

Madison [23.78]. Its validity depends on the point of rating<br />

for a homologous series of air-moving devices. For<br />

such a series, it is useful <strong>to</strong> define dimensionless parameters,<br />

the pressure coefficient ψ and the flow coefficient<br />

φ as:<br />

2P<br />

ψ = , (23.37)<br />

2 ρ (π DN)<br />

φ = Q<br />

π D3 , (23.38)<br />

N<br />

where D is a characteristic dimension (diameter), and<br />

N is the rotational speed of the device. Then, the performance<br />

curve for any device in the series can be expressed<br />

Noise 23.2 Noise Sources 985<br />

as a single curve of ψ versus φ and the operating point<br />

discussed above becomes the point of rating for the<br />

series.<br />

The sound law is then<br />

W = Ws × P2 Q<br />

P2 0 Q0<br />

, (23.39)<br />

where Ws is the specific sound power, and W is the<br />

radiated sound power of the device P0 and Q0 are 1 Pa<br />

and 1 m 3 /s, respectively.<br />

No frequency dependence was given in (23.39), but<br />

values of Ws are often published in octave bands. It must<br />

be emphasized that (23.39) is valid only at a given point<br />

of rating. If the operating point goes from shu<strong>to</strong>ff (P = 0)<br />

<strong>to</strong> free discharge (Q = 0), the point of rating is changing,<br />

and the radiated sound power does not go <strong>to</strong> zero at these<br />

extremes; in fact, it generally increases, as illustrated in<br />

Fig. 23.17. The above sound law is most useful in the<br />

design of large systems when the system resistance is<br />

known and the air-moving device operates near its point<br />

of maximum static efficiency. Using (23.37), (23.38),<br />

and (23.39), it can be shown that at a given point-ofrating,<br />

the sound power is proportional <strong>to</strong> the fifth power<br />

of the speed of the device.<br />

For small air-moving devices, it is most meaningful<br />

<strong>to</strong> obtain sound power level data on the device itself,<br />

usually as a function of speed, operating point, or both.<br />

An apparatus for determination of sound power of small<br />

devices has been standardized both nationally and internationally<br />

[23.79,80]andisshowninFig.23.18 [23.81].<br />

The AMD is mounted on a flexible membrane for airborne<br />

noise tests. Small fans mounted on lightweight<br />

structures are known <strong>to</strong> transmit energy in<strong>to</strong> the structure,<br />

which can then be radiated as sound. The same test<br />

apparatus can also be used for evaluation of the structureborne<br />

vibration of small AMDs if the membrane is<br />

replaced by a specially designed plate [23.82].<br />

Relative A-weighted sound power level (dB)<br />

3.50<br />

3.00<br />

2.50<br />

2.00<br />

1.50<br />

1.00<br />

0.50<br />

0<br />

0.020<br />

0.040<br />

0.060<br />

0.080 0.100 0.120<br />

Flow rate (m 3 /s)<br />

Fig. 23.17 An illustration of relative sound power level as<br />

a function of flow for a small air-moving device<br />

Part G 23.2

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