<?xml version="1.0" encoding="UTF-8"?><?xml-stylesheet type="text/xsl" href="static/style.xsl"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-09-19T09:30:25Z</responseDate><request verb="GetRecord" identifier="oai:drum.lib.umd.edu:1903/24734" metadataPrefix="dim">https://api.drum.lib.umd.edu/server/oai/request</request><GetRecord><record><header><identifier>oai:drum.lib.umd.edu:1903/24734</identifier><datestamp>2022-03-12T08:30:31Z</datestamp><setSpec>com_1903_2206</setSpec><setSpec>com_1903_1654</setSpec><setSpec>com_1903_2</setSpec><setSpec>col_1903_2737</setSpec><setSpec>col_1903_3</setSpec></header><metadata><dim:dim xmlns:dim="http://www.dspace.org/xmlns/dspace/dim" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:doc="http://www.lyncode.com/xoai" xsi:schemaLocation="http://www.dspace.org/xmlns/dspace/dim http://www.dspace.org/schema/dim.xsd">
   <dim:field mdschema="dc" element="contributor" qualifier="advisor">Anderson, John D. Jr</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="advisor">Jones, Everett</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="author">Griffin, Michael Douglas</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="publisher">Digital Repository at the University of Maryland</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="publisher">University of Maryland (College Park, Md)</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="department">Aerospace Engineering</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="accessioned">2019-08-23T19:14:52Z</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="available">2019-08-23T19:14:52Z</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="issued">1977</dim:field>
   <dim:field mdschema="dc" element="identifier">https://doi.org/10.13016/0vek-2vuq</dim:field>
   <dim:field mdschema="dc" element="identifier" qualifier="other">ILLiad # 1300423</dim:field>
   <dim:field mdschema="dc" element="identifier" qualifier="uri">http://hdl.handle.net/1903/24734</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="abstract" lang="en_US">The numerical solution for the flowfield established in a spark-&#xd;
ignition internal combustion engine during the four-stroke (intake,&#xd;
compression, power, exhaust) cycle is considered. Only fluid-dynamic&#xd;
effects are treated with combustion simulated by constant- volume heat&#xd;
addition near top-dead-center on the compression stroke. The working&#xd;
fluid is assumed to be air of constant specific heat, with both viscous&#xd;
and inviscid models considered. Two- and three-dimensional engine models&#xd;
are examined, with the three-dimensional models including both rectangular&#xd;
and cylindrical geometries. The difficulties associated with obtaining&#xd;
numerical solutions in cylindrical coordinates for three-dimensional&#xd;
non-axisymmetric problems when the centerline is included in the region&#xd;
of interest are discussed. A new method which avoids the coordinate-&#xd;
singularity problems associated with such cases is presented and used&#xd;
to obtain the first known four-stroke inviscid-flow solution for a&#xd;
three- dimensional cylindrical engine model. Similar results are presented&#xd;
for a three-dimensional rectangular model, and for the first known&#xd;
two-dimensional four-stroke calculation for a viscous fluid. The inviscid&#xd;
three-dimensional results are compared with each other and with&#xd;
previously obtained two-dimensional inviscid-flow calculations. The use&#xd;
of two-dimensional models is found to be justified for the non- reacting&#xd;
flowfields considered, since the results obtained from a two-dimensional&#xd;
calculation in the valve plane are apparently not strongly dependent on&#xd;
the flowfield perpendicular to the valve plane. It is found that significant&#xd;
flowfields do exist in all I.C. engine models considered. It is&#xd;
shown that the unit-cell-Reynolds-number criterion limits viscous flow&#xd;
calculations to Reynolds numbers of approximately one ten-thousandth&#xd;
the realistic value, and that this produces flowfields which are strongly&#xd;
piston-dominated. In contrast, inviscid results show marked circulatory&#xd;
patterns, which are more realistic. The velocity patterns which develop&#xd;
in the three-dimensional cylindrical engine model are shown to exhibit&#xd;
a marked swirl in planes parallel and perpendicular to the cylinder&#xd;
axis.</dim:field>
   <dim:field mdschema="dc" element="language" qualifier="iso" lang="en_US">en</dim:field>
   <dim:field mdschema="dc" element="title" lang="en_US">Numerical Solutions for Two- and Three-Dimensional Non-Reacting Flowfields in an Internal Combustion Engine</dim:field>
   <dim:field mdschema="dc" element="type" lang="en_US">Dissertation</dim:field>
   <dim:field mdschema="others" element="access-status">open.access</dim:field>
</dim:dim>
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