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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 />

GPB engine simulation model (continued)<br />

wave reflections at end <strong>of</strong> pipe (after time stop)<br />

cylinder, atmosphere or plenum, 155-156<br />

discussion, 154-155<br />

"h<strong>and</strong>," determination <strong>of</strong>, 154-155<br />

restricted pipe, 155<br />

wave transmission (during time increment dt),<br />

147<br />

Harl<strong>and</strong> & Wolff<br />

cathedral engine (diesel), 3, 5<br />

Heat losses<br />

See Heat transfer<br />

Heat release<br />

compression-ignition engines<br />

combustion chamber geometry, 316-317<br />

direct-ignition (DI) engine, 314-316<br />

fast fuel vs. fast air approach, 314<br />

heat loss by fuel vaporization, 308-309<br />

indirect-injection (IDI) engine, 316-318<br />

Woschni heat transfer equation, 305<br />

frictional (in pressure wave propagation), 82-83<br />

SI engines<br />

combustion chamber geometry, 289, 290<br />

heat loss by fuel vaporization, 308<br />

heat release/heat loss calculations, 291-293<br />

incremental heat loss (where QR is zero), 292<br />

incremental heat release (First-Law expression<br />

for), 291, 293<br />

incremental heat release (Rassweiler <strong>and</strong><br />

Winthrow expression for), 293<br />

from loop-scavenged QUB LS400 SI engine,<br />

294, 295<br />

Nusselt number, 305-306, 376<br />

polytropic exponents, determination <strong>of</strong>, 292,<br />

293<br />

prediction from cylinder pressure diagram,<br />

289-294<br />

Reynolds number, 306<br />

in stratified charging/combustion, 468<br />

thermodynamic equilibrium analysis, 291-293<br />

total heat released, 31, 309-310<br />

see also Combustion processes; Heat transfer<br />

Heat transfer<br />

along duct during time step (GPB model)<br />

introduction, 156<br />

604<br />

First Law <strong>of</strong> Thermodynamics, application <strong>of</strong>,<br />

156-158, 160<br />

gas dynamic parameters, values <strong>of</strong> (for four<br />

cases), 158-159<br />

"h<strong>and</strong>" <strong>of</strong> the flow, 160<br />

mass/energy transport diagram (mesh J, four<br />

cases), 156-157<br />

mesh J, energy flow diagram for, 156-157<br />

new reference conditions, determination <strong>of</strong>,<br />

161-162<br />

purity in mesh space J, 161<br />

system state, change <strong>of</strong>, 160<br />

in cylinders <strong>and</strong> plenums during time step (GPB<br />

model)<br />

introduction, 162<br />

boundary conditions, application <strong>of</strong>, 163-164<br />

First Law <strong>of</strong> Thermodynamics, application <strong>of</strong>,<br />

163-165<br />

heat transfer coefficient, determination <strong>of</strong><br />

(discussion), 164<br />

heat transfer from/to plenum, expression for,<br />

164<br />

new gas properties, purity, 166<br />

new reference conditions (for next time step),<br />

166<br />

open cycle flow through cylinder (thermodynamic<br />

diagram), 163<br />

sign conventions, importance <strong>of</strong>, 163<br />

system state, change <strong>of</strong>, 164<br />

system temperature, solution for, 165<br />

heat losses in GPB engine simulation model,<br />

151<br />

heat transfer analysis (Ann<strong>and</strong> model)<br />

closed cycle model (general), 305-307<br />

crankcase analysis, 375-378<br />

heat transfer coefficients, 307-308<br />

racing motorcycle engine, 397-399<br />

Nusselt number in<br />

defined, 84-85<br />

in convection heat transfer analysis, 84-85<br />

in crankcase heat transfer analysis, 376<br />

in open cycle flow through a cylinder<br />

First Law <strong>of</strong> Thermodynamics, application <strong>of</strong>,<br />

163-164<br />

during pressure wave propagation, 84-85<br />

Reynolds number in<br />

in convective heat transfer analysis, 84-85<br />

I

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