Engineering Acoustics. Malcolm J. Crocker

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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 Ir in Eq. (3.41). Figure 3.8 shows two different enclosing surfaces that can be used to determine the sound power of a source. The sound intensity In must 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, Δr, 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.

Schematic illustrations of the sound intensity In, 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. Schematic illustration of sound intensity probe microphone arrangement commonly used.

      Example 3.8

      Solution

      Assuming that ρ = 1.21 kg/m3 and c = 343 m/s, so ρc = 415 ≈ 400 rayls:

equation

      then from Eq. (3.47):

equation equation

      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/m2), what is the sound power of the exhaust source at this frequency?

      Solution

      From Eq. (3.41) images (for an omnidirectional source). Then W = 1.26 × 10−3 watts (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:

      (3.49)equation

      and by taking 10 log throughout this equation

      where Lp is the sound pressure level, LW is the source sound power level, and r is the distance, in metres, from the source center. (Note we have assumed here that ρc = 415 ≅400 rayls.) If ρc ≅ 400 rayls (kg/m2s), then since I = p2rms/ρc

equation

      So,

      (3.51)equation

equation

equation

      (3.52)equation

      where LW is the sound power level of the source and r is the distance in metres.

Schematic illustration of source above a rigid surface.

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