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Design and Simulation of Two Stroke Engines

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 />

TIME, seconds<br />

SUDDEN CONTRACTION<br />

0.00 0.01 0.02 0.03 0.04 0.05<br />

Fig. 2.39 Measured <strong>and</strong> calculated pressures at station I.<br />

0.06<br />

1.10<br />

SUDDEN CONTRACTION<br />

O<br />

b<br />

<<br />

LU<br />

DC<br />

1.05<br />

CO 1.00<br />

CO<br />

LU<br />

DC<br />

Q_<br />

0.95<br />

TIME, seconds<br />

0.00 0.01 0.02 0.03 0.04 0.05 0.06<br />

gi.i<br />

LU<br />

DC<br />

Z)<br />

1.2<br />

CO •) n<br />

n u<br />

CO<br />

Fig. 2.40 Measured <strong>and</strong> calculated pressures at station 2.<br />

MEASURED<br />

LU<br />

MEASURED-<br />

DC<br />

Q-<br />

0.9<br />

TIME, seconds<br />

0.00 0.01 0.02 0.03 0.04 0.05 0.06<br />

Fig. 2.41 Measured <strong>and</strong> calculated pressures at station 3.<br />

the original exhaust pulse <strong>of</strong> 1.06 atm, but the wave proceeding to the outlet has been contracted<br />

from a 80-mm-diameter pipe into a 25-mm tail-pipe.<br />

It can be observed that the GPB finite system modeling gives a very accurate representation<br />

<strong>of</strong> the measured events for the reflection <strong>of</strong> compression pressure waves at sudden decreases<br />

in pipe area.<br />

180

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