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Design and Simulation of Two Stroke Engines

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Chapter 4 - Combustion in <strong>Two</strong>-<strong>Stroke</strong> <strong>Engines</strong><br />

VOLUME CHANGE, \l^ TO V2<br />

TEMPERATURE CHANGE, T-| TO T2<br />

PRESSURE CHANGE, pj TO p2<br />

SQR ^r***^<br />

PISTON MOVES dx<br />

F/g. 4.3 Thermodynamic system during combustion.<br />

work done on the piston is 8W during the time interval. The First Law <strong>of</strong> Thermodynamics<br />

for this closed system states that, during this time step, such events are related by:<br />

SQR - SQL = U2 - UI + 6W (4.2.2)<br />

Where m is the mass <strong>of</strong> gas in the cylinder <strong>and</strong> Cy is the specific heat at constant volume,<br />

the internal energy change is approximately given by:<br />

U2-Ui = mCv(T2-Ti) (4.2.3)<br />

The word approximately is used above, as the value <strong>of</strong> the specific heat at constant volume<br />

is a function <strong>of</strong> temperature <strong>and</strong> also <strong>of</strong> the gas properties. During combustion both the<br />

gas properties <strong>and</strong> the temperatures are varying rapidly, such as several hundreds <strong>of</strong> degrees<br />

Kelvin per degree crankshaft, <strong>and</strong> thus Cy is not a constant as is evident from the discussion<br />

in Sec. 2.1.6. In any arithmetic application <strong>of</strong> Eq. 4.2.3, it is required to employ a value <strong>of</strong> Cy<br />

at some particular state condition such as at either Ti or T2 <strong>and</strong> at the gas properties pertaining<br />

at state condition 1 or 2, or at the mean <strong>of</strong> those two values <strong>and</strong> at the mean <strong>of</strong> the gas<br />

properties pertaining at state condition 1 <strong>and</strong> 2. The simplest method is to employ the properties<br />

at state condition 1, as it will always be a known condition; the properties at T2 are<br />

usually what is being forecast <strong>and</strong> therefore are "unknowns." This caution will not be repeated<br />

throughout the thermodynamic analysis; it will be taken as read that it is included<br />

within the theory being discussed.<br />

The pressure <strong>and</strong> temperature values at each point can be derived through the equation <strong>of</strong><br />

state as:<br />

p2V2 = mRT2 <strong>and</strong> piVi = mRTj (4.2.4)<br />

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