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Introduction to Acoustics

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124 Part A Propagation of Sound<br />

Part A 4.6<br />

the roughness axes, may be written [4.66]<br />

�<br />

3V 2k3 ��<br />

b<br />

β ≈<br />

1 +<br />

2<br />

δ2<br />

�<br />

+ iVk(δ − 1) , (4.38)<br />

2<br />

where V is the roughness volume per unit area of surface<br />

(equivalent <strong>to</strong> mean roughness height), b is the<br />

mean center-<strong>to</strong>-center spacing, δ is an interaction fac<strong>to</strong>r<br />

depending on the roughness shape and packing density<br />

and k is the wave number. An interesting consequence<br />

of (4.38) is that a surface that would be acoustically<br />

hard if smooth has, effectively, a finite impedance at<br />

grazing incidence when rough. The real part of the admittance<br />

allows for incoherent scatter from the surface<br />

and varies with the cube of the frequency and the square<br />

of the roughness volume per unit area. The same approach<br />

can be extended <strong>to</strong> give the effective normalized<br />

surface admittance of a porous surface containing 2-D<br />

roughness [4.65, 69]. For a randomly rough porous surface<br />

near grazing incidence [4.70] it is possible <strong>to</strong> obtain<br />

the following approximation:<br />

� �� �<br />

〈H〉Rs 2 �<br />

Zr ≈ Zs −<br />

− 1 , Re(Zr) ≥ 0<br />

γρ0c0 ν � ,<br />

(4.39)<br />

Corrected level difference (dB re 19 m)<br />

–5<br />

0<br />

5<br />

10<br />

15<br />

20<br />

25<br />

10<br />

100<br />

1 × 10 4<br />

1 × 10 3<br />

Frequency (Hz)<br />

Fig. 4.6 Parkin and Scholes data for the level difference<br />

between microphones at a height of 1.5 m and at distances<br />

of 19 m and 347 m from a fixed jet engine source (nozzlecenter<br />

height 1.82 m) corrected for wavefront spreading<br />

and air absorption. � and ♦ represent data over airfields<br />

(grass covered) at Radlett and Hatfield respectively with<br />

a positive vec<strong>to</strong>r wind between source and receiver of<br />

1.27 m/s (5ft/s); × represent data obtained over approximately<br />

0.15 m thick (6–9 inch) snow at Hatfield and a<br />

positive vec<strong>to</strong>r wind of 1.52 m/s(6ft/s). (After [4.67, 68])<br />

where ν = 1 + 2 3 π〈H〉, 〈H〉 is the root mean square<br />

roughness height and Zs is the impedance of the<br />

porous surface if it were smooth. This can be used<br />

with an impedance model or measured smooth surface<br />

impedance <strong>to</strong> predict the effect of surface roughness for<br />

long wavelengths.<br />

Potentially, cultivation practices have important influences<br />

on ground effect since they change the surface<br />

properties. Aylor [4.71] noted a significant change in<br />

the excess attenuation at a range of 50 m over a soil<br />

after disking without any noticeable change in the meteorological<br />

conditions. Another cultivation practice is<br />

sub-soiling, which is intended <strong>to</strong> break up soil compaction<br />

300 mm or more beneath the ground surface<br />

caused, for example, by the repeated passage of heavy<br />

vehicles. It is achieved by creating cracks in the compacted<br />

layer by means of a single- or double-bladed<br />

tine with sharpened leading edges. Sub-soiling only has<br />

a small effect on the surface profile of the ground. Plowing<br />

turns the soil surface over <strong>to</strong> a depth of about 0.15 m.<br />

Measurements taken over cultivated surfaces before and<br />

after sub-soiling and plowing have been shown <strong>to</strong> be consistent<br />

with the predicted effects of the resulting changes<br />

in surface roughness and flow resistivity [4.65, 72].<br />

4.6.6 Examples of Ground Attenuation<br />

under Weakly Refracting Conditions<br />

Pioneering studies of the combined influences of ground<br />

surface and meteorological conditions [4.67, 68] were<br />

carried out using a fixed Rolls Royce Avon jet engine as<br />

a source at two airfields. The wind speeds and temperatures<br />

were moni<strong>to</strong>red at two heights and therefore it was<br />

possible <strong>to</strong> deduce something about the wind and temperature<br />

gradients during the measurements. However,<br />

perhaps because the role of turbulence was not appreciated<br />

(Sect. 4.8.3), the magnitude of turbulence was not<br />

moni<strong>to</strong>red. This was the first research <strong>to</strong> note and quantify<br />

the change in ground effect with type of surface.<br />

Examples of the resulting data, quoted as the difference<br />

between sound pressure levels at 19 m (the reference<br />

location) and more distant locations corrected for the<br />

decrease expected from spherical spreading and air<br />

absorption, are shown in Fig. 4.6. During slightly downwind<br />

conditions with low wind speed (< 2ms −1 )and<br />

small temperature gradients (< 0.01 ◦ /m), the ground<br />

attenuation over grass-covered ground at Hatfield, although<br />

still a major propagation fac<strong>to</strong>r of more than<br />

15 dB near 400 Hz, was less than that over the other<br />

grass-covered ground at Radlett and its maximum value<br />

occurred at a higher frequency. Snowfall during the pe-

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