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<title>OH PLIF image collection</title>


<p align="center" class="style13"><strong>OH PLIF image collection</strong></p>
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            <p><span class="style5"><strong>Freestream conditions: </strong></span><br />
              M = 2.4 <br />
              p = 40 kPa <br />
              T = 1500 K</p>
            <p align="justify"><span class="style5">Injection: </span><br />
              Hydrogen is injected perpendicularly to the crossflow on a flat plate from a contoured nozzle injector. Injection is sonic. The injector has a diameter D = 2 mm and it is located about 65 mm downstream of the leading edge of the plate. A schematic diagram of the injector is shown in the following figure.</p>
            <p align="center"><img src="fc82a.png" width="520" height="353" /></p>
            <p><span class="style5"><strong>Coordinate system: </strong></span><br />
              x - stream-wise direction <br />
              y - wall-normal direction <br />
              z - span-wise direction</p>
            <p><span class="style5"><strong>Comments: </strong></span><br />
              The coordinate axis have been normalized by the jet diameter. Consistent image corrections (background subtraction, laser sheet correction and dewarping) and colormap have been applied to all cases in order to approximately reconstruct the relative intensity of each case.</p>
            <p class="style5"><strong>Case J = 0.27 </strong><br />
              z/d = 0</p>
            <p align="center"><img src="59354.png" width="520" height="141" /></p>
            <p align="left" class="style5">z/d = 5<br />
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            <p align="center"><img src="0659c.png" width="520" height="141" /></p>
            <p align="left" class="style5"><strong>Case J = 0.68 </strong><br />
              z/d = 0</p>
            <p align="center"><img src="6d1b9.png" width="520" height="141" /></p>
            <p align="left" class="style5">z/d = 5</p>
            <p align="center"><img src="044f1.png" width="520" height="141" /></p>
            <p align="left" class="style5">Case J = 1.77 <br />
              z/d = 0</p>
            <p align="center"><img src="83f60.png" width="520" height="141" /></p>
            <p align="left" class="style5">z/d = 5</p>
            <p align="center"><img src="b1176.png" width="520" height="141" /></p>
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      <p><strong>Groups </strong></p>
      <ul>
        <li><a href="http://psaap.stanford.edu/qmu/Full_System_QMU.html">Full System QMU</a> (Iaccarino) </li>
        <li><a href="http://psaap.stanford.edu/qmu/Computational_Infrastructure.html">Computational Infrastructure</a> (Ham) </li>
        <li><a href="http://psaap.stanford.edu/qmu/solution_verification.html">Solution Verification &amp; Adjoints</a> (Alonso/Duraisamy) </li>
        <li><a href="http://psaap.stanford.edu/heat_release_modeling/index.html">Heat Release Modeling</a> (Terrapon) </li>
        <li><a href="http://psaap.stanford.edu/qmu/Shock_Dynamics_Modeling.html">Shock dynamics Modeling</a> (Lele) </li>
        <li><a href="http://psaap.stanford.edu/qmu/Fuel_Injection_Modeling.html">Fuel Injection Modeling</a> (Cappelli) </li>
        <li><a href="http://psaap.stanford.edu/qmu/Flight_Characterization.html">Flight Characterization</a> (Alonso/Iaccarino) </li>
        <li><a href="http://psaap.stanford.edu/qmu/Thermal_Management.html">Thermal Management</a> (Boyd)</li>
      </ul>
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<p align="center">&nbsp;</p>
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    <BLOCKQUOTE cite="" type="cite" align="center">&nbsp;</BLOCKQUOTE>
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