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Design and Simulation of Two Stroke Engines

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<strong>Design</strong> <strong>and</strong> <strong>Simulation</strong> <strong>of</strong> <strong>Two</strong>-<strong>Stroke</strong> <strong>Engines</strong><br />

Hence, the overall mean square sound pressure, Ps, can be obtained by simple addition <strong>of</strong><br />

that <strong>of</strong> the harmonics, using the procedure for the addition <strong>of</strong> sound energy in Eq. 8.1.5.<br />

How successful that can be may be judged from some <strong>of</strong> the results presented by Coates<br />

[8.3], although that work was carried out using the "homentropic method <strong>of</strong> characteristics"<br />

for the unsteady gas flow along the duct, <strong>and</strong> employed isentropic pipe end boundary conditions,<br />

both <strong>of</strong> which approaches are shown by Kirkpatrick [2.41, 5.20, 5.21] to be <strong>of</strong> a lesser<br />

accuracy than the method presented in Chapter 2. The implication <strong>of</strong> that statement is that<br />

Coates' ability to accurately calculate mass flow rates at the pipe exit, upon which accurate<br />

noise computation is predicated, is impaired. Consequently, this research work is ongoing at<br />

QUB using the theory given in Chapter 2, to investigate the order <strong>of</strong> improvement, if any, in<br />

accuracy <strong>of</strong> prediction <strong>of</strong> noise transmitted into space from the ducting <strong>of</strong> engines.<br />

8.4.2 The experimental work <strong>of</strong> Coates [8.3J<br />

The experimental rig used by Coates is described clearly in Ref. [8.3], but a summary<br />

here will aid the discussion <strong>of</strong> the experimental results <strong>and</strong> their correlation with the theoretical<br />

calculations. The exhaust system is simulated by a rotary valve that allows realistic exhaust<br />

pressure pulses <strong>of</strong> cold air to be blown down into a pipe system at any desired cyclic<br />

speed for those exhaust pressure pulsations. The various pipe systems attached to the exhaust<br />

simulator are shown in Fig. 8.2, <strong>and</strong> are defined as SYSTEMS 1-4. Briefly, they are as follows:<br />

SYSTEM 1 is a plain, straight pipe <strong>of</strong> 28.6 mm diameter, 1.83 m long <strong>and</strong> completely<br />

unsilenced.<br />

SYSTEM 2 has a 1.83 m plain pipe <strong>of</strong> 28.6 mm diameter culminating in what is termed a<br />

diffusing silencer which is 305 mm long <strong>and</strong> 76 mm diameter. The tail-pipe, <strong>of</strong> equal size to<br />

the entering pipe, is 152 mm long.<br />

SYSTEM 3 is almost identical to SYSTEM 2 but has the entry <strong>and</strong> exit pipes re-entering<br />

into the diffusing silencer so that they are 102 mm apart within the chamber.<br />

SYSTEM 4 has what is defined as a side-resonant silencer placed in the middle <strong>of</strong> the<br />

1.83 m pipe, <strong>and</strong> the 28.6-mm-diameter through-pipe has 40 holes drilled into it <strong>of</strong> 3.18 mm<br />

diameter.<br />

More formalized sketches <strong>of</strong> diffusing, side-resonant <strong>and</strong> absorption silencers are found<br />

in Figs. 8.7-8.9. Further discussion <strong>of</strong> their silencing effect, based on an acoustic analysis, is<br />

in Sec. 8.5. It is sufficient to remark at this juncture that:<br />

(i) The intent <strong>of</strong> a diffusing silencer is to absorb all noise at frequencies other than<br />

those at which the box will resonate. Those frequencies which are not absorbed are<br />

called the pass-b<strong>and</strong>s.<br />

(ii) The intent <strong>of</strong> a side-resonant silencer is to completely absorb noise <strong>of</strong> a specific<br />

frequency, such as the fundamental exhaust pulse frequency <strong>of</strong> an engine.<br />

(iii) The intent <strong>of</strong> an absorption silencer is to behave as a diffusing silencer, but to have<br />

the packing absorb the resonating noise at the pass-b<strong>and</strong> frequencies.<br />

The pressure-time histories within these various systems, <strong>and</strong> the one-third octave noise<br />

spectrograms emanating from these systems, were recorded. Of interest are the noise spectra<br />

<strong>and</strong> these are shown for SYSTEMS 1-4 in Figs. 8.3-8.6, respectively. The noise spectra are<br />

presented in the units <strong>of</strong> overall sound pressure level, dBlin, as a function <strong>of</strong> frequency. There<br />

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