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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 />

<strong>of</strong> gas constant, Ru, specific heat at constant volume, Cyy, <strong>and</strong> the ratio <strong>of</strong> specific heats, yu,<br />

may also be determined from Sec. 2.1.6. The average properties <strong>of</strong> the entire cylinder space at<br />

the commencement <strong>of</strong> the time step, <strong>and</strong> which are assumed to prevail during it, may be found<br />

as:<br />

Rl = BiRb - (1 - B,)RU<br />

Cvi = BAb - (1 - B!)CVU<br />

(A4.2.5)<br />

(A4.2.6)<br />

Y^Btfb-fl-Bifru (A4.2.7)<br />

Using heat release data, or a mass fraction burned approach as described in Sec. 4.4.2, the<br />

overall behavior for the entire cylinder space may be found as before, using Eq. 4.4.1, or even<br />

more simply below if the time interval is sufficiently short. A sufficiently short time interval<br />

is defined as 1 ° crankshaft.<br />

T SQR-oQL+meC^-p^-V!)<br />

12 ~<br />

m C<br />

c vl<br />

(A4.2.8)<br />

<strong>and</strong> p2 = ° 1 2 (A4.2.9)<br />

V 2<br />

For the properties within the two zones, a simple solution is possible only if some assumption<br />

is made regarding inter-zone heat transfer. Without such an assumption, it is not<br />

possible to determine the individual volumes within each zone, <strong>and</strong> hence the determination<br />

<strong>of</strong> individual zone temperatures cannot be conducted, as the thermodynamic equation <strong>of</strong> state<br />

must be satisfied for each <strong>of</strong> them, thus:<br />

Tn2=*£f- <strong>and</strong> Tb2=A (A4.2.10)<br />

m R<br />

u2 u<br />

m R<br />

b2 b<br />

Some researchers [4.29-4.31] have employed the assumption that there is zero heat transfer<br />

between the zones during combustion. This is clearly unrealistic, indeed it is inter-zonal<br />

heat transfer which induces detonation. The first simple assumption which can be made to<br />

instill some realism into the solution is that the process in the unburned zone is adiabatic. At<br />

first sight this also appears too naive, but this is not the case as the alternative restatement <strong>of</strong><br />

the adiabatic assumption is that the unburned zone is gaining as much heat from the burned<br />

zone as it is losing to the surfaces <strong>of</strong> the cylinder <strong>and</strong> the piston crown. The more this assumption<br />

is examined, in terms <strong>of</strong> the relative masses, volumes, surface areas <strong>and</strong> temperatures <strong>of</strong><br />

the two zones, the more logical it becomes. With it, the solution is straightforward:<br />

348

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