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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 />

The deflector chamber, type (d)<br />

The calculation for the squish flow area, Asq, is as follows. The flow will be along the<br />

axis <strong>of</strong> the cylinder <strong>and</strong> across the width <strong>of</strong> the deflector, <strong>and</strong> if the flow is considered to take<br />

place midway through the incremental step, then:<br />

— Y .I Y J.<br />

A„„ = xd xs + ' - I (4.5.11)<br />

"sq<br />

where xj is the deflector width.<br />

It is clear that even for equal values <strong>of</strong> csq, higher squish velocities will be given for those<br />

chambers with more <strong>of</strong>fset.<br />

It is also possible to determine the turbulence energy induced by this flow, on the assumption<br />

that it is related to the kinetic energy created. The incremental kinetic energy value at<br />

each time step is dKESq, where:<br />

2<br />

dKEsq=dmsq^- (4.5.12)<br />

The total value <strong>of</strong> turbulence kinetic energy squished, KEsq, is then summed for all <strong>of</strong> the<br />

calculation increments over the compression process from trapping to tdc.<br />

4.5.2 Evaluation <strong>of</strong> squish velocity by computer<br />

The equations in Sec. 4.5.1 are programmed in Prog.4.1, SQUISH VELOCITY, available<br />

from SAE. All <strong>of</strong> the combustion chamber types shown in Fig. 4.13 can be h<strong>and</strong>led by this<br />

program. You are prompted to type in the chamber type by name, either "central," "<strong>of</strong>fset,"<br />

"total <strong>of</strong>fset," or "deflector." Of course, there will appear a design for a combustion chamber<br />

which is not central, yet is not sufficiently <strong>of</strong>fset as to be described by category (b) in Fig.<br />

4.13. Such a chamber would be one where there is still a significant radial clearance from the<br />

bore edge so that the squish flow can proceed in a radial fashion around the periphery <strong>of</strong> the<br />

bowl. In that case, <strong>and</strong> it is one requiring user judgment, the "chamber type?" prompt from the<br />

computer program should be answered with "central."<br />

A typical output from the program is shown in Fig. 4.14, where all <strong>of</strong> the relevant data<br />

input values are observed, with the output values for maximum squish velocity <strong>and</strong> maximum<br />

squish pressure ratio at the crank angle position determined for these maxima, <strong>and</strong> the total<br />

kinetic energy which has been squished. The screen picture is dynamic, i.e., the piston moves<br />

from trapping to tdc, <strong>and</strong> the squish velocity graph is also dynamically created. By such<br />

means the operator obtains an enhanced design feel for the effect <strong>of</strong> squish action, for it is<br />

upon such insight that real design experience is built.<br />

The sketch <strong>of</strong> the engine, cylinder, <strong>and</strong> cylinder head which appears on the screen is<br />

drawn to scale, although the head is drawn as a "bathtub" type purely for ease <strong>of</strong> presentation.<br />

Thus, the physical changes incurred by altering bore-stroke ratio, squish area ratio, squish<br />

clearance, exhaust port timing <strong>and</strong> trapped compression ratio are immediately obvious to the<br />

designer at the same time as the squish velocity characteristics.<br />

330

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