Malcolm J. Crocker - Engineering Acoustics

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Engineering Acoustics: краткое содержание, описание и аннотация

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A comprehensive evaluation of the basic theory for acoustics, noise and vibration control together with fundamentals of how this theoretical material can be applied to real world problems in the control of noise and vibration in aircraft, appliances, buildings, industry, and vehicles. The basic theory is presented in elementary form and only of sufficient complication necessary to solve real practical problems. Unnecessary advanced theoretical approaches are not included. In addition to the fundamental material discussed, chapters are included on human hearing and response to noise and vibration, acoustics and vibration transducers, instrumentation, noise and vibration measurements, and practical discussions concerning: community noise and vibration, interior and exterior noise of aircraft, road and rail vehicles, machinery noise and vibration sources, noise and vibration in rapid transit rail vehicles, automobiles, trucks, off road vehicles, and ships. In addition, extensive up to date useful references are included at the end of each chapter for further reading. The book concludes with a glossary on acoustics, noise and vibration

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(3.45) Engineering Acoustics - изображение 274

The dipole is obviously a much less efficient radiator than a monopole, particularly at low frequency.

Example 3.7

Two monopoles of equal sound power W = 0.1 watt at 150 Hz, but pulsating with a phase difference of 180° are spaced λ /12 apart. Determine the sound power of this dipole at 150 Hz.

Solution

We know that l = λ /12, λ = 343/150 = 2.29 m, and W m= 0.1 watt. If we compare the sound power of a dipole W dwith that of a monopole W m( Eqs. (3.44)and (3.45)) we find that

Therefore the sound power radiated by the dipole is 9 mW In practical - фото 275

Therefore, the sound power radiated by the dipole is 9 mW.

In practical situations with real directional sound sources and where background noise and reflections are important, use of Eq. (3.43)becomes difficult and less accurate, and then the sound power is more conveniently determined from Eq. (3.41)with a sound intensity measurement system. See Ref. [22] in this book and chapter 106 in the Handbook of Acoustics [1].

We note that since p/u r= ρc (where ρ = mean air density kg/m 3and c = speed of sound 343 m/s) for a plane wave or sufficiently far from any source, that

(3.46) where Eq 346is true for random noise as well as for a singlefrequency - фото 276

where Eq. (3.46)is true for random noise as well as for a single‐frequency sound, known as a pure tone.

Note that for such cases we only need to measure the mean‐square sound pressure with a simple sound level meter (or at least a simple measurement system) to obtain the sound intensity from Eq. (3.46)and then from that the sound power W watts from Eq. (3.41)is

(3.47) for an omnidirectional source monopole with no reflections and no background - фото 277

for an omnidirectional source (monopole) with no reflections and no background noise. This result is true for noise signals and pure tones that are produced by omnidirectional sources and in the so‐called far acoustic field.

For the special case of a pure‐tone (single‐frequency) source of sound pressure amplitude, Engineering Acoustics - изображение 278, we note that Engineering Acoustics - изображение 279and Engineering Acoustics - изображение 280from Eq. (3.47).

For measurements on a hemisphere, W = 2 πr 2 p 2 rms /ρc and for a pure‐tone source Engineering Acoustics - изображение 281, and Engineering Acoustics - изображение 282, from Eq. (3.47).

Note that in the general case, the source is not omnidirectional, or more importantly, we must often measure quite close to the source so that we are in the near acoustic field, not the far acoustic field. However, if appreciable reflections or background noise (i.e. other sound sources) are present, then we must measure the intensity I rin Eq. (3.41). Figure 3.8shows two different enclosing surfaces that can be used to determine the sound power of a source. The sound intensity I nmust always be measured perpendicular (or normal) to the enclosing surfaces used. Measurements are normally made with a two‐microphone probe (see Ref. [22]). The most common microphone arrangement is the face‐to‐face model (see Figure 3.9).

The microphone arrangement shown also indicates the microphone separation distance, Δ r , needed for the intensity calculations [22]. In the face‐to‐face arrangement a solid cylindrical spacer is often put between the two microphones to improve the performance.

Figure 38 Sound intensity I n being measured on a segment dS of an - фото 283

Figure 3.8 Sound intensity I n, being measured on (a) segment dS of an imaginary hemispherical enclosure surface and (b) an elemental area dS of a rectangular enclosure surface surrounding a source having a sound power W .

Figure 39 Sound intensity probe microphone arrangement commonly used - фото 284

Figure 3.9 Sound intensity probe microphone arrangement commonly used.

Example 3.8

By making measurements around a source (an engine exhaust pipe) it is found that it is largely omnidirectional at low frequency (in the range of 50–200 Hz). If the measured sound pressure level on a spherical surface 10 m from the source is 60 dB at 100 Hz, which is equivalent to a mean‐square sound pressure p 2 rmsof (20 × 10 −3) 2(Pa) 2, what is the sound power in watts at 100 Hz frequency?

Solution

Assuming that ρ = 1.21 kg/m 3and c = 343 m/s, so ρc = 415 ≈ 400 rayls:

then from Eq 347 Example 39 - фото 285

then from Eq. (3.47):

Example 39 If the sound intensity level measured using a sound intensity - фото 286 Example 39 If the sound intensity level measured using a sound intensity - фото 287

Example 3.9

If the sound intensity level, measured using a sound intensity probe at the same frequency, as in Example 3.8, but at 1 m from the exhaust exit, is 80 dB (which is equivalent to 0.0001 W/m 2), what is the sound power of the exhaust source at this frequency?

Solution

From Eq. (3.41) for an omnidirectional source Then W 126 10 3watts the same result as - фото 288(for an omnidirectional source). Then W = 1.26 × 10 −3watts (the same result as Example 3.8).

Sound intensity measurements do and should give the same result as sound pressure measurements made in a free field.

Far away from omnidirectional sound sources, provided there is no background noise and reflections can be ignored:

(3.48) 349 and by taking 10 log throughout this equation 350 - фото 289

(3.49) and by taking 10 log throughout this equation 350 where L pis the sound - фото 290

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