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  <title><![CDATA[MS Defense by Ezekiel M. Bugay]]></title>
  <body><![CDATA[<p>&nbsp;</p>

<p><span><span><span><strong><span><span>Ezekiel M. Bugay</span></span></strong><br />
<em><span><span>(Advisor: Dr. Wenting Sun]</span></span></em></span></span></span></p>

<p><span><span><span><em><span><span>will defend a master's thesis entitled,</span></span></em></span></span></span></p>

<p><span><span><span><strong><span><span>Characterization of Nanoparticle Soot Size</span></span></strong></span></span></span></p>

<p><span><span><span><strong><span><span>Distribution from an Aero-Derivative Combustor </span></span></strong></span></span></span></p>

<p><span><span><span><strong><span><span>by use of Half-Mini DMA</span></span></strong></span></span></span></p>

<p><span><span><span><em>On</em></span></span></span></p>

<p><span><span><span><strong>Friday, August 4th at 8:00 a.m.<br />
Montgomery Knight Building 317</strong></span></span></span><br />
&nbsp;</p>

<p><span><span><span><span><strong><span><span>Abstract<br />
&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></strong>Developing carbon nanoparticles resulting from flames, known as nascent soot, has come under increasing scrutiny with regards to combustion engines and systems because of its direct contribution to non-volatile particulate matter (nvPM) emissions, which are a major global pollutant. A realistic Rich-Burn, Quick-Mix, Lean-Burn (RQL) aero-derivative combustion test rig was constructed with the intent of measuring and characterizing sub-10nm soot nanoparticle size distributions utilizing a state-of-the-art differential mobility analyzer (DMA, Half-Mini #p model) at a variety of operating conditions. Methodologies, design alterations, and results are proposed for global equivalence ratios between 0.1-0.2 and combustion pressures between 35-85 psi. The data obtained suggests qualitative evidence that higher combustion pressures result in generally less species above 6nm, until 85 psi when a widening of the size distribution was noted. Future work is suggested to refine the methodology and collect a larger library of data to improve certainties.</span></span></span></span></p>

<p><span><span><span><strong>Committee</strong></span></span></span></p>

<ul>
	<li><span><span><span>Dr. Wenting Sun– School of Aerospace Engineering (advisor)</span></span></span></li>
	<li><span><span><span>Dr. Adam M. Steinberg– School of Aerospace Engineering</span></span></span></li>
	<li><span><span><span>Dr. Ellen Yi Chen Mazumdar– School of Mechanical Engineering</span></span></span></li>
</ul>
]]></body>
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<p><span><span><span><strong><span><span>Distribution from an Aero-Derivative Combustor </span></span></strong></span></span></span></p>

<p><span><span><span><strong><span><span>by use of Half-Mini DMA</span></span></strong></span></span></span></p>
]]></value>
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