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    <link>http://localhost:8080/xmlui/handle/123456789/2703</link>
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    <pubDate>Tue, 23 Jun 2026 06:28:28 GMT</pubDate>
    <dc:date>2026-06-23T06:28:28Z</dc:date>
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      <title>Local heat transfer for jet impingement onto a concave surface including injection nozzle length to diameter and curvature ratio effects</title>
      <link>http://localhost:8080/xmlui/handle/123456789/2704</link>
      <description>Title: Local heat transfer for jet impingement onto a concave surface including injection nozzle length to diameter and curvature ratio effects
Authors: patil, V. S.
Abstract: The effect of jet nozzle length to diameter ratio on local heat transfer coefficient measurements for a row of&#xD;
circular jets impinging onto a concave surface for varying target spacing are reported here. The nozzle length to&#xD;
diameter ratio (L/d) and the nozzle to target spacing (H/d) were varied from 0.2 to 6 and 0.67 to 8 respectively.&#xD;
Three curvature ratios, defined as the ratio of jet diameter to target surface diameter (d/D), equal to 0.1, 0.2 and&#xD;
0.3 were studied and the jet to jet pitch to diameter ratio (P/d) was kept constant at 4.0. The Reynolds number&#xD;
was varied between 10,000 and 50,000 and wall static pressures for some cases were measured for obtaining a&#xD;
better understanding of the heat transfer coefficient variations.&#xD;
Higher stagnation zone Nusselt numbers were observed for the jet nozzles with small L/d at small H/d values&#xD;
whereas at larger H/d values nozzle length was observed to affect the data only marginally. The difference&#xD;
between Nusselt number values, between H/d = 2 and H/d =8, was observed to progressively reduce with&#xD;
increasing L/d ratio and this was true for both the local stagnation point as well as the spanwise averaged&#xD;
stagnation line values. The maximum local Nusselt number values were observed to shift from the geometric&#xD;
impingement location to nearby locations for very small nozzle diameter to target distance ratios (H/d≤ 1) for&#xD;
larger curvature ratios. A constant heat transfer impingement area with constant pumping power criterion is&#xD;
presented to compare the performance of the different configurations studied. The longer nozzle lengths and&#xD;
smaller curvature ratios are observed to perform better based on this criterion. A correlation is presented for the&#xD;
overall averaged Nusselt number, with a validity within the parameter range studied, with a±10% error band</description>
      <pubDate>Fri, 04 Aug 2017 00:00:00 GMT</pubDate>
      <guid isPermaLink="false">http://localhost:8080/xmlui/handle/123456789/2704</guid>
      <dc:date>2017-08-04T00:00:00Z</dc:date>
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