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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 />

The values <strong>of</strong> X* X,, ao, ce, <strong>and</strong> q were 1.0264, 0.9686, 343.1, 45.3, <strong>and</strong> 53.9, respectively,<br />

in terms <strong>of</strong> a positive direction for the transmission <strong>of</strong> each wave. In other words, the<br />

properties <strong>of</strong> waves pe <strong>and</strong> pj are to be assigned to waves 1 <strong>and</strong> 2, respectively, merely to<br />

reduce the arithmetic clutter both within the text <strong>and</strong> in your mind.<br />

If pi is regarded as moving rightward <strong>and</strong> that is defined as the positive direction, <strong>and</strong><br />

consequently, p2 is moving leftward as in a negative direction, then Eqs. 2.2.1 <strong>and</strong> 2.2.2 show:<br />

Hence,<br />

Xs = Xi + X2 - 1 = 1.0264 - 0.9868 - 1 = 0.995<br />

ps = xs 7 = 0.965 <strong>and</strong> ps = Psp0 = 0.965 x 101,325 = 97,831 Pa<br />

cs = 45.3 + [-(-53.9)] = 99.2 m/s<br />

Thus, the pressure transducer in the wall <strong>of</strong> the pipe would show little <strong>of</strong> this process, as<br />

the summation <strong>of</strong> the two waves would reveal a trace virtually indistinguishable from the<br />

atmospheric line, <strong>and</strong> exhibit nothing <strong>of</strong> the virtual doubling <strong>of</strong> the particle velocity.<br />

The opposite effect takes place when two waves <strong>of</strong> the same type undergo a superposition<br />

process. For example, if wave pi met another wave pi going in the other direction <strong>and</strong> in the<br />

plane <strong>of</strong> the pressure transducer, then:<br />

Xs = 1.0264 + 1.0264 - 1 = 1.0528 <strong>and</strong> Ps = xj = 1.0528 7 = 1.434<br />

cs = 45.3 + [-(445.3)] = 0 m/s<br />

The pressure transducer would show a large compression wave with a pressure ratio <strong>of</strong><br />

1.434 <strong>and</strong> tell nothing <strong>of</strong> the zero particle velocity at the same spot <strong>and</strong> time.<br />

This makes the interpretation <strong>of</strong> exhaust <strong>and</strong> intake pressure records a most difficult<br />

business if it is based on experimentation alone. Not unnaturally, the engineering observer<br />

will interpret a measured pressure trace which exhibits a large number <strong>of</strong> pressure oscillations<br />

as being evidence <strong>of</strong> lots <strong>of</strong> wave activity. This may well be so, but some <strong>of</strong> these<br />

fluctuations will almost certainly be periods approaching zero particle velocity also while yet<br />

other periods <strong>of</strong> this superposition trace exhibiting "calm" could very well be operating at<br />

particle velocities approaching the sonic value! As this is clearly a most important topic, it<br />

will be returned to in later sections <strong>of</strong> this chapter.<br />

2.2.2 Wave propagation during superposition<br />

The propagation velocity <strong>of</strong> the two waves during the superposition process must also<br />

take into account direction. The statement below is accurate for the superposition condition<br />

where the rightward direction is considered positive.<br />

where, as = aoXs<br />

72

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