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        <identifier>oai:www.ideals.illinois.edu:2142/83998</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>Dutton, J. Craig</dc:contributor>
          <dc:contributor>Lucht, Robert P.</dc:contributor>
          <dc:creator>Woodmansee, Mark Allen</dc:creator>
          <dc:date>2015-09-25T21:13:04Z</dc:date>
          <dc:date>2015-09-25T21:13:04Z</dc:date>
          <dc:date>10000-01-01</dc:date>
          <dc:date>1999</dc:date>
          <dc:date>1999</dc:date>
          <dc:description>In the underexpanded jet flowfield, the experimental P/T/p measurements are compared to similar quantities extracted from a RANS CFD simulation. The agreement between the mean CARS measurements and CFD predictions along the jet centerline and radial traverses is generally excellent. This CARS technique is able to capture the low-pressure and low-temperature conditions of the M = 3.4 flow entering the Mach disk, as well as the conditions immediately downstream of this normal shock. Further downstream, both the CARS and CFD temperature distributions corroborate the existence of concentric inner and outer shear layers. The former evolves from a slip line that separates the subsonic inner jet fluid from the surrounding annulus of supersonic fluid. Similarly, the existence of counter-rotating streamwise-oriented vortices may explain the slight deviations of the CARS pressure measurements from the CFD pressure distribution in the outer compressible shear layer.</dc:description>
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  Previous issue date: 1999</dc:description>
          <dc:description>Embargo set by: Seth Robbins for item 85279
Lift date: Forever
Reason: Restricted to the U of I community idenfinitely during batch ingest of legacy ETDs</dc:description>
          <dc:description>Restricted to the U of I community idenfinitely during batch ingest of legacy ETDs</dc:description>
          <dc:description>U of I Only</dc:description>
          <dc:description>225 p.</dc:description>
          <dc:description>Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1999.</dc:description>
          <dc:identifier>http://hdl.handle.net/2142/83998</dc:identifier>
          <dc:identifier>(MiAaPQ)AAI9953178</dc:identifier>
          <dc:language>eng</dc:language>
          <dc:subject>Engineering, Aerospace</dc:subject>
          <dc:title>Experimental Measurements of Pressure, Temperature, and Density Using High-Resolution N(2) Coherent Anti-Stokes Raman Scattering</dc:title>
          <dc:type>text</dc:type>
          <degree>
            <department>Mechanical Engineering</department>
            <discipline>Mechanical Engineering</discipline>
            <grantor>University of Illinois at Urbana-Champaign</grantor>
            <level>Dissertation</level>
            <name>Ph.D.</name>
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