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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 />

Mass flow rate = density x area x velocity = psAcs<br />

where, ps = p0Xs G5 (2.2.11)<br />

Hence, rfi = G5a0p0A(X1 + X2 - l) G5 (X1 - X2) (2.2.12)<br />

In terms <strong>of</strong> the numerical example used in Sec. 2.2.2, the values <strong>of</strong> ao, po, Xi, <strong>and</strong> X2<br />

were 343.1, 1.2049, 1.0264, <strong>and</strong> 0.9686, respectively. The pipe area is that <strong>of</strong> the 25-mmdiameter<br />

duct, or 0.000491 m 2 . The gas in the pipe is air.<br />

We can solve for the mass flow rate by using the previously known value <strong>of</strong> Xs, which<br />

was 0.995, or that for particle velocity cs which was 99.2 m/s, <strong>and</strong> determine the superposition<br />

density ps thus:<br />

ps = p0X G5 = 1.2049 x 0.995 5 = 1.1751 kg/m 3<br />

Hence, the mass flow rate during superposition is given by:<br />

m right = 1-1751 x 0.000491 x 99.2 = 0.0572 kg/s<br />

The sign was known by having available the information that the superposition particle<br />

movement was rightward <strong>and</strong> inserting cs as +99.2 <strong>and</strong> not -99.2. Alternatively, the formal<br />

Eq. 2.2.12 gives a numeric answer indicating direction <strong>of</strong> mass or particle flow. This is obtained<br />

by solving Eq. 2.2.12 with the lead term in any bracket, i.e., X]j as that value where<br />

wave motion is considered to be in a positive direction.<br />

Hence, mass flow rate rightward. as direction <strong>of</strong> wave 1 is called positive, is:<br />

bright = G 5aoPoA(X! + X2 - l) G5 (X1 - X2)<br />

= 5x 343.11 x 1.2049 x (1.0264 + 0.9686 - 1) x (1.0264 - 0.9686) 5<br />

= +0.0572 kg/s<br />

It will be observed, indeed it is imperative to satisfy the equation <strong>of</strong> continuity, that the<br />

superposition mass flow rate is the sum <strong>of</strong> the mass flow rate induced by the individual waves.<br />

The mass flow rates in a rightward direction <strong>of</strong> waves 1 <strong>and</strong> 2, computed earlier in Sec. 2.1.4,<br />

were 0.0305 <strong>and</strong> 0.0272 kg/s, respectively.<br />

2.2.4 Supersonic particle velocity during wave superposition<br />

In typical engine configurations it is rare for the magnitude <strong>of</strong> finite amplitude waves<br />

which occur to provide a particle velocity that approaches the sonic value. As the Mach<br />

number M is defined in Eq. 2.1.23 for a pressure amplitude ratio <strong>of</strong> X as:<br />

74

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