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Design and Simulation of Two Stroke Engines

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gas constant/universal gas constant, 64<br />

mass ratios (oxygen, nitrogen), 65<br />

molal enthalpy, internal energy, 65<br />

molal specific heat (at constant pressure, volume),<br />

65<br />

molal specific heats (oxygen, nitrogen), 66<br />

molecular weight, average, 65<br />

specific heat (at constant pressure, temperature),<br />

64<br />

specific heats ratio, 64<br />

Gaussian Elimination method<br />

for wave reflection at contractions in pipes, 107<br />

for wave reflection at outflow from a cylinder,<br />

132<br />

General Motors<br />

diesel road engines, 3<br />

Geometric compression ratio, defined, 8<br />

GPB engine simulation model<br />

introduction<br />

unsteady gas flow computation, discussion <strong>of</strong>,<br />

142-144<br />

basis <strong>of</strong> GPB model, 144<br />

computational model, criteria for, 143-144<br />

duct meshing for pressure wave propagation,<br />

144-145<br />

four-stroke engines, applicability to, 143<br />

GPB model computational requirements, 145<br />

physical parameters (e.g., pressure, density,<br />

etc.), 145<br />

pressure wave propagation within mesh J<br />

(illus.), 146<br />

Reimann variables, use <strong>of</strong>, 142<br />

superposition pressure amplitude ratio, 145<br />

air flow into an engine<br />

B parameter, assessment <strong>of</strong>, 167<br />

delivery ratio, 168<br />

scavenge ratio, 168<br />

total mass air flow, 167<br />

computation time, comments on, 191-192<br />

concluding remarks about, 192<br />

correlation with QUB SP experimental appara<br />

tus. See under QUB (Queen's University <strong>of</strong><br />

Belfast)<br />

friction <strong>and</strong> heat, changes due to, 151<br />

inter-mesh boundaries (reflections after time<br />

stop)<br />

introduction, 151-152<br />

603<br />

Index<br />

adjacent meshes in differing discontinuities<br />

(diagram), 152<br />

parallel ducting, 152-153<br />

tapered pipes, 153-154<br />

interpolation procedure (wave transmission<br />

through a mesh)<br />

gas dynamic parameters, values <strong>of</strong>, 149-150<br />

groupings <strong>of</strong> variables ("known" terms), 148<br />

pressure amplitude ratios, determination <strong>of</strong>,<br />

148-149<br />

propagation velocities, 147<br />

singularities during interpolation procedure,<br />

150<br />

values <strong>of</strong> lengths xp> xq 147<br />

mass/energy transport along duct (after time<br />

stop)<br />

introduction, 156<br />

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

156-158, 160<br />

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

cases), 158-159<br />

"h<strong>and</strong>" <strong>of</strong> the flow, 157<br />

mesh J, energy flow diagram for, 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 />

transport at mesh J (four cases), 156-157<br />

thermodynamics <strong>of</strong> cylinders <strong>and</strong> plenums (during<br />

time step)<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 />

time interval, selection <strong>of</strong>, 146

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