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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 />

those that are the supplied pipes, at any junction. For an n-pipe junction, that is basically the<br />

only addition to the theory below other than that the number <strong>of</strong> equations increases by the<br />

number <strong>of</strong> extra junctions. With the mathematical technique <strong>of</strong> solution by the Newton-Raphson<br />

method for multiple polynomial equations, <strong>and</strong> the matrix arithmetic h<strong>and</strong>led by the Gaussian<br />

Elimination method, the additional computational complexity is negligible.<br />

The sign convention for particle flow is declared as "positive" toward the branch <strong>and</strong> Fig.<br />

2.13 inherently stipulates that convention. The pressure loss criterion for flow from one branch<br />

to another is set out by Bingham as,<br />

Ap = CLpsC2 (2.14.1)<br />

where the loss coefficient CL is given by the inter-branch angle 9,<br />

C L = 1-6 " -— if 9 > 167 then CL = 0 (2.14.2)<br />

167<br />

In any branch there are supplier pipes <strong>and</strong> supplied pipes. There are two possibilities in<br />

this regard <strong>and</strong> these lead to two assumptions for their solution. The more fundamental assumption<br />

in much <strong>of</strong> the theory is that the gas within the pipes is a mixture <strong>of</strong> two gases <strong>and</strong><br />

in an engine context this is logically exhaust gas <strong>and</strong> air. Obviously, the theory is capable <strong>of</strong><br />

being extended to a mixture <strong>of</strong> many gases, as indeed air <strong>and</strong> exhaust gas actually are. Equally,<br />

the theory is capable <strong>of</strong> being extended relatively easily to branches with any number <strong>of</strong> pipes<br />

at the junction. The theory set out below details a three-way branch for greater ease <strong>of</strong> underst<strong>and</strong>ing.<br />

(a) One supplier pipe<br />

Here there is one supplier pipe <strong>and</strong> two are being supplied, in which case the solution<br />

required is for the reflected wave amplitudes, Xr, in all three pipes <strong>and</strong> for the reference<br />

acoustic velocities, ao, for the gas going toward the two supplied pipes. The word "toward" is<br />

used here precisely. This means there are five unknown values needing five equations. It is<br />

possible to reduce this number <strong>of</strong> unknowns by one, if we assume that the reference acoustic<br />

state toward the two supplied pipes is common. A negligible loss <strong>of</strong> accuracy accompanies<br />

this assumption. Using the notation <strong>of</strong> Fig. 2.13, it is implied that pipe 1 is supplying pipes 2<br />

<strong>and</strong> 3; that notation will be used here only to "particularize" the solution so as to aid underst<strong>and</strong>ing<br />

<strong>of</strong> the analysis. As the pressure in the face <strong>of</strong> pipes 2 <strong>and</strong> 3 will be normally very<br />

close, the difference between TQ2 <strong>and</strong> T03 should be small <strong>and</strong>, as the reference acoustic<br />

velocity is related to the square root <strong>of</strong> these numbers, the error is potentially even smaller.<br />

Irrespective <strong>of</strong> that assumption, it follows absolutely that the basic properties <strong>of</strong> the gas entering<br />

the supplied pipes is that <strong>of</strong> the supplier pipe.<br />

(b) <strong>Two</strong> supplier pipes<br />

Here there is one supplied pipe <strong>and</strong> two are suppliers, in which case the solution required<br />

is for the reflected wave amplitudes, Xr, in all three pipes <strong>and</strong> for the reference acoustic<br />

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