15.02.2013 Views

Design and Simulation of Two Stroke Engines

Design and Simulation of Two Stroke Engines

Design and Simulation of Two Stroke Engines

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

<strong>Design</strong> <strong>and</strong> <strong>Simulation</strong> <strong>of</strong> <strong>Two</strong>-<strong>Stroke</strong> <strong>Engines</strong><br />

P2<br />

T2<br />

P2<br />

C2<br />

A2<br />

Pr2<br />

-Pi2<br />

Fig. 2.76 Outflow from a cylinder or plenum to a pipe.<br />

The solution <strong>of</strong> the gas dynamics <strong>of</strong> the flow must include separate treatments for subsonic<br />

outflow <strong>and</strong> sonic outflow. The first presentation <strong>of</strong> the solution for this type <strong>of</strong> flow<br />

was by Wallace <strong>and</strong> Nassif [2.5] <strong>and</strong> their basic theory was used in a computer-oriented<br />

presentation by Blair <strong>and</strong> Cahoon [2.6]. Probably the earliest <strong>and</strong> most detailed exposition <strong>of</strong><br />

the derivation <strong>of</strong> the equations involved is that by McConnell [2.7]. However, while all <strong>of</strong><br />

these presentations declared that the flow was analyzed non-isentropically, a subtle error was<br />

introduced within the analysis that negated that assumption. Moreover, all <strong>of</strong> the earlier solutions,<br />

including that by Bingham [2.19], used fixed values <strong>of</strong> the cylinder properties throughout<br />

<strong>and</strong> solved the equations with either the properties <strong>of</strong> air (y = 1.4 <strong>and</strong> R = 287 J/kgK) or<br />

exhaust gas (y = 1.35 <strong>and</strong> R = 300 J/kgK). The arithmetic solution was stored in tabular form<br />

<strong>and</strong> indexed during the course <strong>of</strong> a computation. Today, that solution approach is inadequate,<br />

for the precise equations in fully non-isentropic form must be solved at each instant <strong>of</strong> a<br />

computation for the properties <strong>of</strong> the gas which exists at that location at that juncture.<br />

Since a more complex solution, i.e., that for restricted pipes in Sect. 2.12, has already<br />

been presented, the complete solution for outflow from a cylinder or plenum in an unsteady<br />

gas-dynamic regime will not pose any new theoretical difficulties.<br />

The case <strong>of</strong> subsonic particle flow will be presented first <strong>and</strong> that for sonic flow is given<br />

in Sec. 2.16.1.<br />

In Fig. 2.16 the exp<strong>and</strong>ing flow from the throat to the downstream superposition point 2<br />

is seen to leave turbulent vortices in the corners <strong>of</strong> that section. That the streamlines <strong>of</strong> the<br />

flow give rise to particle flow separation implies a gain <strong>of</strong> entropy from the throat to area<br />

section 2. On the other h<strong>and</strong>, the flow from the cylinder to the throat is contracting <strong>and</strong> can be<br />

considered to be isentropic in the same fashion as the contractions debated in Sees. 2.11 <strong>and</strong><br />

2.12. This is summarized on the temperature-entropy diagram in Fig. 2.17 where the gain <strong>of</strong><br />

entropy for the flow rising from pressure pt to pressure pS2 is clearly visible. The isentropic<br />

nature <strong>of</strong> the flow from pi to pt, a vertical line on Fig. 2.17, can also be observed.<br />

The properties <strong>and</strong> composition <strong>of</strong> the gas particles are those <strong>of</strong> the gas at the exit <strong>of</strong> the<br />

cylinder to the pipe. The word "exit" is used most precisely. For most cylinders <strong>and</strong> plenums<br />

128

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!