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Design and Simulation of Two Stroke Engines

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Chapter 2 - Gas Flow through <strong>Two</strong>-<strong>Stroke</strong> <strong>Engines</strong><br />

What is evident, however, is that during any simulation <strong>of</strong> unsteady gas flow or <strong>of</strong> the<br />

thermodynamic processes within engines, it is imperative for its accuracy to use the correct<br />

value <strong>of</strong> the gas properties at all locations within the engine.<br />

2.2 Motion <strong>of</strong> oppositely moving pressure waves in a pipe<br />

In the previous section, you were asked to conduct an imaginary experiment with Fred,<br />

who produced compression <strong>and</strong> expansion waves by exhaling or inhaling sharply, producing<br />

a "boo" or a "u...uh," respectively. Once again, you are asked to conduct another experiment<br />

so as to draw on your experience <strong>of</strong> sound waves to illustrate a principle, in this case the<br />

behavior <strong>of</strong> oppositely moving pressure waves. In this second experiment, you <strong>and</strong> your friend<br />

Fred are going to say "boo" at each other from some distance apart, <strong>and</strong> af the same time.<br />

Each person's ears, being rather accurate pressure transducers, will record his own "boo"<br />

first, followed a fraction <strong>of</strong> time later by the "boo" from the other party. Obviously, the "boo"<br />

from each passed through the "boo" from the other <strong>and</strong> arrived at both Fred's ear <strong>and</strong> your ear<br />

with no distortion caused by their passage through each other. If distortion had taken place,<br />

then the sensitive human ear would have detected it. At the point <strong>of</strong> meeting, when the waves<br />

were passing through each other, the process is described as "superposition." The theoretical<br />

treatment below is for air, as this simplifies the presentation <strong>and</strong> enhances your underst<strong>and</strong>ing<br />

<strong>of</strong> the theory; the extension <strong>of</strong> the theory to the generality <strong>of</strong> gas properties is straightforward.<br />

2.2.1 Superposition <strong>of</strong> oppositely moving waves<br />

Fig. 2.3 illustrates two oppositely moving pressure waves in air in a pipe. They are shown<br />

as compression waves, ABCD <strong>and</strong> EFGH, <strong>and</strong> are sketched as being square in pr<strong>of</strong>ile, which<br />

is physically impossible but it makes the task <strong>of</strong> mathematical explanation somewhat easier.<br />

In Fig. 2.3(a) they are about to meet. In Fig. 2.3(b) the process <strong>of</strong> superposition is taking place<br />

for the front EF on wave top BC, <strong>and</strong> for the front CD on wave top FG. The result is the<br />

creation <strong>of</strong> a superposition pressure, ps, from the separate wave pressures, pi <strong>and</strong> p2. Assume<br />

that the reference acoustic velocity is ao- Assuming also that the rightward direction is mathematically<br />

positive, the particle <strong>and</strong> the propagation velocity <strong>of</strong> any point on the wave top,<br />

BC, will be ci <strong>and</strong> ah From Eqs. 2.1.18-20:<br />

ci=5ao(Xi-l) ai=ao(6Xi-5)<br />

Similarly, the values for the wave top FG will be (with rightward regarded as the positive<br />

direction):<br />

c2 = -5a0(X2 - 1) a2 = -ao(6X2 - 5)<br />

From Eq. 2.1.14, the local acoustic velocities in the gas columns BE <strong>and</strong> DG during<br />

superposition will be:<br />

ai = arjXi a2 = arjX2<br />

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