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Design and Simulation of Two Stroke Engines

Design and Simulation of Two Stroke Engines

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Chapter 5 - Computer Modeling <strong>of</strong> <strong>Engines</strong><br />

Nevertheless, the explanation <strong>of</strong> the mechanism <strong>of</strong> the achievement <strong>of</strong> high specific performance<br />

characteristics in the simple, ported two-stroke engine is quite straightforward. The<br />

fundamental principles are (i) provide a "plugging" pulse prior to trapping to seal in the<br />

cylinder charge <strong>and</strong> prevent spillage, (ii) provide a "suction" pulse around the bdc position to<br />

assist the scavenging flow in reaching a high charging efficiency prior to sealing, (iii) provide<br />

a "suction" pulse around the bdc position to extract air from the crankcase <strong>and</strong> lower its<br />

pressure so as to commence induction vigorously, <strong>and</strong> (iv) harness the exhaust pulse resonance<br />

effects to enhance the basic mechanisms <strong>of</strong> (i), (ii) <strong>and</strong> (iii), if that is possible within<br />

the design configuration. This process is significantly related to engine speed, as the further<br />

illustrations from this simulation <strong>of</strong> cylinder <strong>and</strong> exhaust pipe pressure show in Figs. 6.18 to<br />

6.20 for engine speeds <strong>of</strong> 9600, 11,200 <strong>and</strong> 12,300 rpm, respectively. They are near the bottom,<br />

near the peak, <strong>and</strong> at the upper end <strong>of</strong> the useful power b<strong>and</strong> <strong>of</strong> this highly tuned engine.<br />

The basic tuning <strong>and</strong> charging action seen in Fig. 5.32 is observed to appear in Figs. 6.18-6.20<br />

to a greater or lesser degree. Further discussion occurs in Sec. 6.2.5 with respect to the design<br />

<strong>of</strong> the expansion chambers for two-stroke engines <strong>and</strong> their speed-related tuning characteristics.<br />

A discussion on speed-related tuning is also in Sec. 6.2.5.<br />

The behavior <strong>of</strong> the reed valve induction system, Fig. 5.35<br />

Fig. 5.35 shows the results <strong>of</strong> computer simulation <strong>of</strong> the reed valve motion, the delivery<br />

ratio, <strong>and</strong> the forcing pressures to create those effects, namely within the crankcase <strong>and</strong> the<br />

superposition pressure at the entrance to the reed block which is at the crankcase end <strong>of</strong> the<br />

inlet tract. The reed valve motion is plotted as the tip lift ratio, Crcjt-<br />

It can be seen that the reed is open for most <strong>of</strong> the cycle, but it is impelled into action by<br />

a strong pressure ratio across it which lasts from about 190° atdc to 240° atdc. The pressurecreated<br />

impulse is significant, for it coincides with (i) the crankcase pressure having been<br />

lowered below atmospheric pressure by the gas-dynamic tuning action emanating from the<br />

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