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        <identifier>oai:www.ideals.illinois.edu:2142/70624</identifier>
        <datestamp>2023-07-11</datestamp>
        <setSpec>col_2142_5131</setSpec>
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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:title>An Experimental Study of Single and Multiple Turbulent Buoyant Jets in Crossflow</dc:title>
          <dc:type>text</dc:type>
          <dc:creator>Leylek, Jim A.</dc:creator>
          <dc:date>2014-12-15T23:55:52Z</dc:date>
          <dc:date>2014-12-15T23:55:52Z</dc:date>
          <dc:date>10000-01-01</dc:date>
          <dc:date>1984</dc:date>
          <dc:date>1984</dc:date>
          <dc:description>The phenomenon of turbulent, buoyant jets in crossflow is a fundamental fluid mechanics problem with many application areas, including jets discharged from natural and mechanical draft cooling towers. Buoyant jets have been studied for many years, and as a result there exists a large body of literature on this and other related topics. An extensive review of this literature showed that there was a need for an improved laboratory simulation technique and quantitative data on both single and multiple buoyant jets.</dc:description>
          <dc:description>A new buoyant jet simulation technique is developed which uses a vertically downward discharge of cold nitrogen gas into a wind tunnel with discharge temperature of the jet ranging between -30(DEGREES)C and -150(DEGREES)C. This technique is capable of simulating the puff-like nature of prototype cooling tower plumes as evidenced by flow visualization which is inherent in this method. A large body of data are reported for both single and multiple jets covering a wide range of parameters. Single jet data are obtained for discharge densimetric Frounde number F varying between 0.2 and 2.4 and crossflow-to-exit velocity ratio k varying between 0.2 and 11.7. The multiple jet data are reported for three angles of orientation (theta) with F values varying between 1.1 and 2.7 and k between 0.5 and 3.</dc:description>
          <dc:description>The single jet results show that trajectory is very sensitive to k. The discharge densimetric Froude number also affects the trajectory but to a lesser extent. Temperature decay, on the other hand, is more sensitive to F than it is to k. An increase in k has the effect of lowering the trajectory of the jet. The isotherm downwind extension, which is a measure of effective jet mixing, increases with k for k less than the critical value k(,*). For k &amp;gt; k(,*) this trend reverses, indicating a more enhanced jet mixing. Physically, k(,*) indicates onset of jet/wake interaction. In highly buoyant jets, jet/wake interaction is prolonged until very high k.</dc:description>
          <dc:description>The multiple jets show that the inline configuration ((theta) = 0 degrees) results in considerably high trajectory compared with the oblique and crossflow cases for all F and k combinations encountered in the experiments. The oblique case trajectories are consistently higher than crossflow trajectories for k  k(,*) the oblique case exhibits by far the lowest trajectories. Two mechanisms are identified for having a key role in the behavior of multiple buoyant jets, these are:  (a) jet shielding and (b) jet/wake interaction.</dc:description>
          <dc:description>Made available in DSpace on 2014-12-15T23:55:52Z (GMT). No. of bitstreams: 1
8422115.pdf: 7296253 bytes, checksum: 2d89c01eca6642362ca559468fb72a5a (MD5)
  Previous issue date: 1984</dc:description>
          <dc:description>Embargo set by: Seth Robbins for item 70790
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>270 p.</dc:description>
          <dc:description>Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1984.</dc:description>
          <dc:identifier>http://hdl.handle.net/2142/70624</dc:identifier>
          <dc:identifier>(UMI)AAI8422115</dc:identifier>
          <dc:subject>Physics, Fluid and Plasma</dc:subject>
          <degree>
            <department>Aeronautical and Astronautical Engineering</department>
            <discipline>Aeronautical and Astronautical Engineering</discipline>
            <grantor>University of Illinois at Urbana-Champaign</grantor>
            <level>Dissertation</level>
            <name>Ph.D.</name>
          </degree>
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