29.12.2013 Views

Analysis and Ranking of the Acoustic Disturbance Potential of ...

Analysis and Ranking of the Acoustic Disturbance Potential of ...

Analysis and Ranking of the Acoustic Disturbance Potential of ...

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

Report No. 6945<br />

I<br />

BBN Systems <strong>and</strong> Technologies Corporation<br />

TABLE 3.4<br />

CULTURAL AND RECREAT IOllAL SOURCES<br />

Source Type Darinont BY, Hz Wax 1/3 Oct,Hz Teuq!oral Time Source Level Data<br />

fain fut Lsl,dB freq. Ls2,dB Pattern Ratio )Icas/Est, Referme<br />

24' Outdrive, 2-80HP (20kt) (1) moving 40 16000b 167 500 156 Fluct. 0.L W Maln et 01. 1981<br />

16' Zodiac, ZOHP (20kt) (1) mving 3150 10000 157 6300 152 Fluct. 0.& W Y<br />

13' Uhaler, 20HP (20kt) (1) mving 630 6000 159 4000 153 Fluct. 0.L W Y<br />

Smmchinc(16Mhr)(2) mving 250 2500 130 1600 124 Fluct. O.& E Hollidayetal.1980<br />

Helicopter uanrrcp on ice (2) Local 63 1600 139 160 131 Contin. 1 E dennring <strong>and</strong> Uhi te 1984<br />

Shotgm, 10ga (3) loco l 80 3150 172 500 162 lnpulse 0.005 w BEN Archives.<br />

Notes:<br />

b B<strong>and</strong>width limited by available data<br />

(1) Undcrwter mound<br />

(2) Signatures obtained in wter uwkr ice cover<br />

(3) Airbom soud<br />

source level <strong>of</strong> 167 dB represents <strong>the</strong> upper range <strong>of</strong> source levels for most<br />

recreational sources. This level is comparable to that produced by a 35 m<br />

( 110 ft) twin-screw diesel vessel as shown in Table 3.3A. When several<br />

vessels <strong>of</strong> this type are operating in close proximity <strong>the</strong> cumulative noise<br />

level can reach values similar to those that would be produced by a medium<br />

sized ship.<br />

Example spectra for several <strong>of</strong> <strong>the</strong> more popular airborne sound sources<br />

are shown in Fig. 3.18. Note that <strong>the</strong>se are radiated noise spectra for a<br />

range <strong>of</strong> 150 m, not source level spectra. The snowmobile spectrum is<br />

reresentative <strong>of</strong> older models <strong>and</strong> was obtained during acceleration <strong>of</strong> <strong>the</strong><br />

machine while running at about 40 km/hr (25 mph). The spectrum for <strong>the</strong> 10<br />

gauge shotgun shows peak 1/3 octave b<strong>and</strong> levels. Since this is a highly<br />

sporadic <strong>and</strong> impulsive source it is difficult to estimate a representative<br />

time fraction to obtain an equivalent level. If a pressure pulse time<br />

constant <strong>of</strong> 2 msec <strong>and</strong> a shot repetition rate <strong>of</strong> l/hr is assumed, <strong>the</strong> Leq for<br />

<strong>the</strong> shotgun is est'imated to be about 60 dB less than <strong>the</strong> spectrum levels shown<br />

in Fig. 3.18. The longer duration signal from <strong>the</strong> aircraft flyover thus is<br />

one <strong>of</strong> loudest recreational source signah.

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!