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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 />

particle flow direction<br />

(a) non-isentropic expansion<br />

s1<br />

s2<br />

s1<br />

O/<br />

^<br />

s2<br />

(b) isentropic contraction<br />

Fig. 2.10 Particle flow in simple expansions <strong>and</strong> contractions.<br />

turn equation. The properties <strong>and</strong> composition <strong>of</strong> the gas particles are those <strong>of</strong> the gas at the<br />

upstream point. Therefore, the various functions <strong>of</strong> the gas properties are:<br />

Y = Yi R = Rj G5 = G5i G7 = G7j , etc.<br />

The continuity equation for mass flow in Eq. 2.9.5 is still generally applicable <strong>and</strong> repeated<br />

here, although the entropy gain is reflected in the reference acoustic velocity <strong>and</strong><br />

density at position 2:<br />

This equation becomes:<br />

m1-m2=0 (2.10.1)<br />

.G5<br />

rG5<br />

Pol** A^saoi&i " Xrl) + Po2X£ > A2G5a02(Xi2 - Xr2) = 0 (2.10.2)<br />

The First Law <strong>of</strong> Thermodynamics was introduced for such flow situations in Sec. 2.8.<br />

The analysis required here follows similar logical lines. The First Law <strong>of</strong> Thermodynamics<br />

for flow from superposition station 1 to superposition station 2 can be expressed as:<br />

2 2<br />

u , c sl _ u . c s2<br />

sl ~2~ ~ 2 T"<br />

or, (4+G5ari)-(c?2+G5a?2) = 0 (2.10.3)<br />

102

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