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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 />

column labeled "E or C" describes whether the flow encountered was at an expansion (E) or<br />

a contraction (C) in pipe area.<br />

Table 2.12.3 Output data from the calculations using the more complex theory<br />

No.<br />

1<br />

2<br />

3<br />

4<br />

5<br />

6<br />

Pn<br />

0.8850<br />

0.9036<br />

1.1227<br />

1.1292<br />

1.1371<br />

1.0174<br />

Pf2<br />

1.0785<br />

1.0746<br />

1.3118<br />

1.2886<br />

1.2595<br />

1.0487<br />

mg/s<br />

46.38<br />

43.91<br />

48.70<br />

44.69<br />

39.77<br />

27.98<br />

T02K<br />

294.5<br />

296.2<br />

293.0<br />

295.2<br />

298.1<br />

306.7<br />

Theory<br />

Sec. 2.10<br />

Sec. 2.12<br />

Sec. 2.11<br />

Sec. 2.12<br />

Sec. 2.12<br />

Sec. 2.12<br />

For simple expansions, in test data sets 1 <strong>and</strong> 2, the constant pressure theory works remarkably<br />

well with an almost negligible error, i.e., less than 3% in mass flow rate terms. If the<br />

expansion has a realistic coefficient <strong>of</strong> discharge <strong>of</strong> 0.85 applied to it then that error on mass<br />

flow rate rises slightly from 2.65 to 2.8%. The magnitudes <strong>of</strong> the reflected pressure waves<br />

compare quite favorably in most circumstances.<br />

At a simple sudden contraction in test data sets 3 <strong>and</strong> 4, even with a coefficient discharge<br />

<strong>of</strong> 1.0 the mass flow rate error is significant at 8.2%, rising to 17.9% error when the quite<br />

logical Cd value <strong>of</strong> 0.7 is applied to the sudden contraction. The magnitudes <strong>of</strong> the reflected<br />

pressure waves are significantly different when emanating from the simple <strong>and</strong> the complex<br />

theories.<br />

When any form <strong>of</strong> restriction is placed in the pipe, i.e., in test data sets 5 <strong>and</strong> 6 for an<br />

expansion <strong>and</strong> a contraction, respectively, the constant pressure theory is simply not capable<br />

<strong>of</strong> providing any relevant information either for the magnitude <strong>of</strong> the reflected wave or for the<br />

mass flow rates. The error is greater for expansions than contractions, which is the opposite<br />

<strong>of</strong> the situation when restrictions in the pipe are not present. Note the significant entropy<br />

gains in tests 4-6.<br />

The constant pressure theory is seen to be reasonably accurate only for flow which encounters<br />

sudden expansions in the ducting.<br />

2.13 An introduction to reflections <strong>of</strong> pressure waves at branches in a pipe<br />

The simple theoretical treatment for this situation was also suggested by Benson [2.4]<br />

<strong>and</strong> in precisely the same form as for the sudden area changes found in the previous section.<br />

A sketch <strong>of</strong> a typical branch is shown in Fig. 2.13. The sign convention for all <strong>of</strong> the branch<br />

theory presented here is that inward propagation <strong>of</strong> a pressure wave toward the branch will be<br />

regarded as "positive." Benson [2.4] postulates that the superposition pressure at the junction,<br />

at any instant <strong>of</strong> wave incidence <strong>and</strong> reflection, can be regarded as a constant. This is a<br />

straightforward extension <strong>of</strong> his thinking for the expansion <strong>and</strong> contractions given in Sec. 2.9.<br />

114

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