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Design and Simulation of Two Stroke Engines

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

where Ck is the value <strong>of</strong> the thermal conductivity <strong>of</strong> air at the instantaneous crankcase temperature,<br />

Tcc, <strong>and</strong> consequently may be found from Eq. 2.3.10.<br />

The value <strong>of</strong> Tccw is defined as the average temperature <strong>of</strong> the crankcase wall surface, the<br />

exposed crankshaft <strong>and</strong> connecting rod surfaces, the surface <strong>of</strong> the underside <strong>of</strong> the piston,<br />

<strong>and</strong> the exposed cylinder liner surface. The heat transfer, 5QCC, over a crankshaft angle interval,<br />

d6, <strong>and</strong> a time interval, dt, can be deduced for the mean value <strong>of</strong> that transmitted to the<br />

total surface area exposed to the cylinder gases:<br />

as<br />

dt<br />

d9 60<br />

x<br />

360 rpm<br />

(5.3.5)<br />

then "Qcc - ChAccw(TCc Tccw)dt (5.3.6)<br />

The total surface area within the crankcase, Accw, is composed <strong>of</strong>:<br />

Accw = A.crankcase + Apiston + Acrankshaft (5.3.7)<br />

It is straightforward to exp<strong>and</strong> the heat transfer equation in Eq. 5.3.6 to deal with the<br />

individual components <strong>of</strong> it, by assigning a wall temperature to each specific area noted in<br />

Eq. 5.3.7. It should also be noted that Eq. 5.3.6 produces a "positive" number for the "loss" <strong>of</strong><br />

heat from the cylinder, aligning it with the sign convention assigned in Sec. 4.3.4.<br />

The typical values obtained from the use <strong>of</strong> the above theory are illustrated in Table 5.1.<br />

The example employed is for a two-stroke engine <strong>of</strong> 86 mm bore, 86 mm stroke, running at<br />

4000 rpm with a flywheel diameter <strong>of</strong> 150 mm. Various state conditions for the crankcase gas<br />

throughout the cycle are selected <strong>and</strong> the potential state conditions <strong>of</strong> pressure (in atm units)<br />

<strong>and</strong> temperature (in °C units) are estimated to arrive at the tabulated values for a two-stroke<br />

engine, based on the solution <strong>of</strong> the above equations. The three conditions selected are, in<br />

table order: at st<strong>and</strong>ard atmospheric conditions, at the height <strong>of</strong> crankcase compression, <strong>and</strong><br />

at the peak <strong>of</strong> the suction process.<br />

Table 5.1 Crankcase heat transfer using the Ann<strong>and</strong> model<br />

Pec<br />

(atm)<br />

1.0<br />

1.2<br />

0.6<br />

Tec<br />

(°C)<br />

20<br />

120<br />

60<br />

Nu<br />

1770<br />

1448<br />

1078<br />

Re<br />

299,037<br />

224,483<br />

146,493<br />

ch<br />

(W/m 2 K)<br />

It can be seen that the convection heat transfer coefficient does not vary greatly over the<br />

range <strong>of</strong> operational conditions within the crankcase, but the variation is sufficiently significant<br />

as to warrant the inclusion <strong>of</strong> the analytical technique within an engine simulation. The<br />

377<br />

316<br />

321<br />

210

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