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        <identifier>oai:www.ideals.illinois.edu:2142/101680</identifier>
        <datestamp>2023-07-11</datestamp>
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        <thesis xmlns="http://www.ndltd.org/standards/metadata/etdms/1.1/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:dc="http://purl.org/dc/elements/1.1/" xsi:schemaLocation="http://www.ndltd.org/standards/metadata/etdms/1.1/ http://www.ndltd.org/standards/metadata/etdms/1.1/etdms11.xsd http://purl.org/dc/elements/1.1/ http://www.ndltd.org/standards/metadata/etdms/1.1/etdmsdc.xsd">
          <dc:contributor>Gazzola, Mattia</dc:contributor>
          <dc:creator>Dubey, Vedant</dc:creator>
          <dc:date>2018-09-27T16:30:19Z</dc:date>
          <dc:date>2018-09-27T16:30:19Z</dc:date>
          <dc:date>2020-09-28T09:15:30Z</dc:date>
          <dc:date>2018-07-06</dc:date>
          <dc:date>2018-08</dc:date>
          <dc:description>Computational Fluid Dynamic Solvers for ﬂow structure interaction problems rely on a delicate treatment of ﬂuid and grid properties close to the boundary. Although such an approach is accurate, it proves to be inﬂexible when applied to complex deforming geometries. Here we combine remeshed vortex methods with a panel method to design a new Vortex Fluxing scheme that uses no special treatment of ﬂow properties at the boundary. It was found that the panel method is capable of correcting any spurious vorticity ﬂux into the wall during the no slip boundary application. This enables highly accurate, robust Direct Numerical Simulations by relaxing the need for small timesteps and allowing the use of coarse regular computational grids. The methodology was validated for rigid, rotating and deforming bodies.</dc:description>
          <dc:description>Submission published under a 24 month embargo labeled 'U of I Access', the embargo will last until 2020-08-01</dc:description>
          <dc:description>The student, Vedant Dubey, accepted the attached license on 2018-07-06 at 01:53.</dc:description>
          <dc:description>The student, Vedant Dubey, submitted this Thesis for approval on 2018-07-06 at 02:04.</dc:description>
          <dc:description>This Thesis was approved for publication on 2018-07-06 at 10:35.</dc:description>
          <dc:description>DSpace SAF Submission Ingestion Package generated from Vireo submission #12750 on 2018-09-27 at 11:16:39</dc:description>
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DUBEY-THESIS-2018.pdf: 6418473 bytes, checksum: a347fe74ea9976e2b896c56d595fbeb4 (MD5)
LICENSE.txt: 4209 bytes, checksum: 820159346747effad92786f714e1f993 (MD5)
  Previous issue date: 2018-07-06</dc:description>
          <dc:description>Embargo set by: Seth Robbins for item 107778
Lift date: 2020-09-27T16:30:34Z
Reason: Author requested U of Illinois access only (OA after 2yrs) in Vireo ETD system</dc:description>
          <dc:description>Embargo set by: Seth Robbins for item 107778
Lift date: 2020-09-27T16:31:43Z
Reason: Author requested U of Illinois access only (OA after 2yrs) in Vireo ETD system</dc:description>
          <dc:description>Embargo set by: Seth Robbins for item 107778
Lift date: 2020-09-27T16:34:29Z
Reason: Author requested U of Illinois access only (OA after 2yrs) in Vireo ETD system</dc:description>
          <dc:description>U of I Only Restriction Lifted for Item 107778 on 2020-09-28T09:15:30Z.</dc:description>
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          <dc:identifier>http://hdl.handle.net/2142/101680</dc:identifier>
          <dc:language>en</dc:language>
          <dc:rights>Copyright 2018 by Vedant Dubey. All rights reserved.</dc:rights>
          <dc:subject>Vortex Methods, Self Corrective, Computational Fluid Dynamics, Panel Method, Fluxing</dc:subject>
          <dc:title>A self corrective vortex fluxing method for viscous fluid structure interaction problems</dc:title>
          <dc:type>text</dc:type>
          <dc:type>text</dc:type>
          <degree>
            <department>Aerospace Engineering</department>
            <discipline>Aerospace Engineering</discipline>
            <grantor>University of Illinois at Urbana-Champaign</grantor>
            <level>Thesis</level>
            <name>M.S.</name>
          </degree>
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