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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 />

value <strong>of</strong> XRI for mesh 1. To proceed with the next time step <strong>of</strong> the calculation, the value <strong>of</strong><br />

XLI is required. What then is the value <strong>of</strong> XLI ? The answer, as before, is that it will depend on<br />

what the right-h<strong>and</strong> end <strong>of</strong> the pipe is connected to, i.e., a branch, a restricted pipe, the atmosphere,<br />

etc.<br />

The GPB modeling method stores information regarding the "h<strong>and</strong>" <strong>of</strong> the two end meshes<br />

in every pipe, <strong>and</strong> must be able to index the name <strong>of</strong> that "h<strong>and</strong>" at its connection to its own<br />

discontinuity, so that the numerical result <strong>of</strong> the computation <strong>of</strong> boundary conditions at the<br />

ends <strong>of</strong> every pipe is placed in the appropriate storage location within the computer.<br />

Consider each boundary condition in turn, a restricted pipe, a cylinder, plenum or atmosphere,<br />

<strong>and</strong> a branch.<br />

(a) a restricted pipe, as sketched in Fig. 2.22(c)<br />

Imagine, just as it is sketched, that mesh 1 is at the right-h<strong>and</strong> end <strong>of</strong> pipe 1 <strong>and</strong> that mesh<br />

2 is at the left-h<strong>and</strong> end <strong>of</strong> pipe 2. Thence:<br />

!XR1 = Xpl <strong>and</strong> 2XL = Xq2 (2.18.40)<br />

The unknown quantities are the values <strong>of</strong> the reflected pressure waves, iprj <strong>and</strong> 2PR,<br />

represented here by their pressure amplitude ratios, namely IXLI <strong>and</strong> 2XR. The analytical<br />

solution for these, <strong>and</strong> also for the entropy gain on the downstream side <strong>of</strong> whichever direction<br />

the particle flow takes, is to be found in Sec. 2.12. In terms <strong>of</strong> the notation in Fig. 2.8,<br />

which accompanies the text <strong>of</strong> Sec. 2.12, the value referred to as Xpi is clearly the incident<br />

wave XJI, <strong>and</strong> the value <strong>of</strong> Xq2 is obviously the incident pressure wave Xj2.<br />

(b) a cylinder, plenum, or the atmosphere as sketched in Figs. 2.16 <strong>and</strong> 2.18<br />

A cylinder, plenum, or the atmosphere is considered to be a large "box," sufficiently large<br />

to consider the particle velocity within it to be effectively zero. For the rest <strong>of</strong> this section, a<br />

cylinder, plenum, or the atmosphere will be referred to as a "box." In the theory given in Sees.<br />

2.16 <strong>and</strong> 2.17, the entire analysis is based on knowing the physical geometry at any instant<br />

<strong>and</strong>, depending on whether the flow is inflow or outflow, either the thermodynamic state<br />

conditions <strong>of</strong> the pipe or the "box" are known values.<br />

As previously in this section, the "h<strong>and</strong>" <strong>of</strong> the incident wave at the mesh in the pipe<br />

section adjacent to the cylinder is an important element <strong>of</strong> the modeling process. Imagine that<br />

mesh 1, as shown in Fig. 2.22(a), is that mesh at the left-h<strong>and</strong> end <strong>of</strong> the pipe <strong>and</strong> attached to<br />

the cylinder exactly as it is sketched in either Fig. 2.16 or 2.18. In which case at the end <strong>of</strong> the<br />

time step in computation, to implement the theory given in Sees. 2.16 <strong>and</strong> 2.17, the following<br />

is the nomenclature interconnection for that to occur:<br />

lXL = Xqj (2.18.41)<br />

<strong>and</strong> pi2 = p01xg 7 (2.18.42)<br />

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