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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 />

Pressure wave reflection (in pipes) (continued)<br />

outflow from a cylinder (continued)<br />

temperature-entropy diagrams, 128-129<br />

at restrictions between differing pipe areas<br />

introduction, 108<br />

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

110-112<br />

flow momentum equation, 111, 112<br />

gas properties (functions <strong>of</strong>), 109<br />

mass flow continuity equation, 110, 111<br />

numerical examples, 113-114<br />

particle flow regimes (diagram <strong>of</strong>), 109<br />

reference state conditions, 109<br />

sonic particle velocity, solution for, 112-113<br />

temperature-entropy curves for, 108-109<br />

at sudden area changes<br />

introduction, 97<br />

Benson "constant pressure" criterion, 98-99<br />

energy flow diagram, 98<br />

examples: enlargements <strong>and</strong> contractions,<br />

100-101<br />

nomenclature, consistency <strong>of</strong>, 98<br />

in tapered pipes<br />

introduction, 124-126<br />

dimensions <strong>and</strong> flow diagram, 125<br />

gas particle Mach number, importance <strong>of</strong>, 127<br />

separation <strong>of</strong> flow (from walls), 126-127<br />

Pressure wave superposition (oppositely moving,<br />

in pipes)<br />

introduction, 69<br />

mass flow rate<br />

directional conventions for, 73-74<br />

numerical values <strong>of</strong>, 74<br />

supersonic particle velocity<br />

Mach number (defined), 74-75<br />

numerical values for, 77<br />

Rankine-Hugoniot equations (combined<br />

shock/reflection), 76-77<br />

superposition Mach number (determination<br />

<strong>of</strong>), 75-76<br />

weak shock concept (for modeling unsteady<br />

gas flow), 75, 77<br />

wave propagation<br />

acoustic, propagation velocities (numerical<br />

values for), 73<br />

acoustic velocity, sign conventions for, 73<br />

propagation velocities, sign conventions for,<br />

73<br />

612<br />

"wave interference during superposition" effect,<br />

73<br />

wave superposition<br />

acoustic velocities, local, 69<br />

particle velocity, absolute, 70<br />

particle/propagation velocities, sign conventions<br />

for, 69, 71<br />

particle/propagation velocities (individual<br />

wavetop), 69<br />

pressure-time data, experimental (interpretation<br />

<strong>of</strong>), 71-72<br />

simplified pressure diagram, 70<br />

superposition particle velocity (analytical),<br />

70-71<br />

superposition particle velocity (experimental),<br />

71-72<br />

superposition pressure ratio, 71<br />

Propagation/particle velocity (acoustic waves)<br />

pressure ratio, 54<br />

specific heats ratio (for air), 54<br />

velocity in air (after Earnshaw), 54<br />

Propagation/particle velocity (finite amplitude<br />

waves in free air)<br />

particle velocity<br />

absolute pressure (p), 55<br />

gas constant (for air), 55<br />

gas particle velocity (for air), 55, 57<br />

pressure amplitude ratio, 55<br />

pressure ratio, 55<br />

specific heat (constant pressure/volume), 55<br />

specific heat ratio, functions <strong>of</strong> (for air), 56<br />

specific heats ratio, 55<br />

propagation velocity<br />

absolute propagation velocity, 57-58<br />

acoustic velocity, 57<br />

density, 57<br />

isentropic change <strong>of</strong> state, 57<br />

Propagation/particle velocity (finite amplitude<br />

waves in pipes)<br />

basic parameters (values in air)<br />

particle velocity, 58<br />

pressure amplitude ratio, 58<br />

propagation velocity, 58<br />

reference acoustic velocity, 58, 59<br />

reference density, 59<br />

the compression wave<br />

absolute pressure, 59<br />

density, 60

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