<p>Jet impingement heat transfer (JIHT) is a technique deployed in various cooling/heating applications. The heat transfer (HT) and flow structure of a confined circular air impinging jet on a flat plate with a circular row of novel droplet roughness elements are numerically investigated utilizing the RNG k-ε turbulence model. The effects of Reynolds number in the range between 7,000 and 35,000, the location of the droplet roughness elements (DREs) relative-to-jet diameter (<InlineEquation ID="IEq1"> <EquationSource Format="TEX">\(s/d\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mi>s</mi> <mo stretchy="false">/</mo> <mi>d</mi> </mrow> </math></EquationSource> </InlineEquation>) of 1.5, 2, 2.5, and 3 and confinement plate height (<InlineEquation ID="IEq2"> <EquationSource Format="TEX">\(H/d\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mi>H</mi> <mo stretchy="false">/</mo> <mi>d</mi> </mrow> </math></EquationSource> </InlineEquation>) of 0.25, 0.5, 1, and 1.5 are studied. The distribution of surface temperature, local Nusselt number (<InlineEquation ID="IEq3"> <EquationSource Format="TEX">\(\it {\text{Nu}}\)</EquationSource> <EquationSource Format="MATHML"><math> <mtext mathvariant="italic">Nu</mtext> </math></EquationSource> </InlineEquation>), average Nusselt number (<InlineEquation ID="IEq4"> <EquationSource Format="TEX">\(\it {\text{Nu}}_{{{\text{avg}}}}\)</EquationSource> <EquationSource Format="MATHML"><math> <msub> <mtext mathvariant="italic">Nu</mtext> <mtext mathvariant="italic">avg</mtext> </msub> </math></EquationSource> </InlineEquation>), average Nusselt number ratio (<InlineEquation ID="IEq5"> <EquationSource Format="TEX">\(0\it {\text{Nu}}_{{{\text{avg}}/phantom{i}{\text{.r}}}}\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mn>0</mn> <msub> <mtext mathvariant="italic">Nu</mtext> <mrow> <mtext mathvariant="italic">avg</mtext> <mo stretchy="false">/</mo> <mi mathvariant="italic">phantom</mi> <mi mathvariant="italic">i</mi> <mtext mathvariant="italic">.r</mtext> </mrow> </msub> </mrow> </math></EquationSource> </InlineEquation>), velocity distribution, streamline contours, turbulence kinetic energy (<i>TKE</i>), and static pressure (<InlineEquation ID="IEq6"> <EquationSource Format="TEX">\(p\)</EquationSource> <EquationSource Format="MATHML"><math> <mi>p</mi> </math></EquationSource> </InlineEquation>) drop are discussed. In addition, the performance evaluation criterion (<InlineEquation ID="IEq7"> <EquationSource Format="TEX">\(\it {\text{PEC}}\)</EquationSource> <EquationSource Format="MATHML"><math> <mtext mathvariant="italic">PEC</mtext> </math></EquationSource> </InlineEquation>) is assessed to evaluate the overall performance of the confined jet impingement. The results show that the presence of droplet roughness elements considerably influences the rates of heat transfer. At <InlineEquation ID="IEq8"> <EquationSource Format="TEX">\(s/d\)</EquationSource> <EquationSource Format="MATHML"><math> <mrow> <mi>s</mi> <mo stretchy="false">/</mo> <mi>d</mi> </mrow> </math></EquationSource> </InlineEquation> = 1.5, <i>H/d</i> = 0.5, and <i>Re</i> = 35,000, the <InlineEquation ID="IEq9"> <EquationSource Format="TEX">\(\it {\text{Nu}}_{{{\text{avg}}}}\)</EquationSource> <EquationSource Format="MATHML"><math> <msub> <mtext mathvariant="italic">Nu</mtext> <mtext mathvariant="italic">avg</mtext> </msub> </math></EquationSource> </InlineEquation>, <InlineEquation ID="IEq10"> <EquationSource Format="TEX">\(\it {\text{Nu}}_{{{\text{avg}}/phantom{i}{\text{.r}}}}\)</EquationSource> <EquationSource Format="MATHML"><math> <msub> <mtext mathvariant="italic">Nu</mtext> <mrow> <mtext mathvariant="italic">avg</mtext> <mo stretchy="false">/</mo> <mi mathvariant="italic">phantom</mi> <mi mathvariant="italic">i</mi> <mtext mathvariant="italic">.r</mtext> </mrow> </msub> </math></EquationSource> </InlineEquation><sub><i>,</i></sub> and <InlineEquation ID="IEq11"> <EquationSource Format="TEX">\(\it {\text{PEC}}\)</EquationSource> <EquationSource Format="MATHML"><math> <mtext mathvariant="italic">PEC</mtext> </math></EquationSource> </InlineEquation> equal 127, 2.45, and 2.88, respectively. As well, DREs significantly reduce the recirculation zone downstream of the roughness elements.</p>

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Effect of droplet roughness elements on heat transfer and fluid flow over a plate subjected to a confined air jet

  • Mustafa Abdelfattah,
  • Ahmed Sowayan,
  • Mohamed A. Aziz,
  • Sabbah Ataya,
  • Hussein M. Maghrabie

摘要

Jet impingement heat transfer (JIHT) is a technique deployed in various cooling/heating applications. The heat transfer (HT) and flow structure of a confined circular air impinging jet on a flat plate with a circular row of novel droplet roughness elements are numerically investigated utilizing the RNG k-ε turbulence model. The effects of Reynolds number in the range between 7,000 and 35,000, the location of the droplet roughness elements (DREs) relative-to-jet diameter ( \(s/d\) s / d ) of 1.5, 2, 2.5, and 3 and confinement plate height ( \(H/d\) H / d ) of 0.25, 0.5, 1, and 1.5 are studied. The distribution of surface temperature, local Nusselt number ( \(\it {\text{Nu}}\) Nu ), average Nusselt number ( \(\it {\text{Nu}}_{{{\text{avg}}}}\) Nu avg ), average Nusselt number ratio ( \(0\it {\text{Nu}}_{{{\text{avg}}/phantom{i}{\text{.r}}}}\) 0 Nu avg / phantom i .r ), velocity distribution, streamline contours, turbulence kinetic energy (TKE), and static pressure ( \(p\) p ) drop are discussed. In addition, the performance evaluation criterion ( \(\it {\text{PEC}}\) PEC ) is assessed to evaluate the overall performance of the confined jet impingement. The results show that the presence of droplet roughness elements considerably influences the rates of heat transfer. At \(s/d\) s / d  = 1.5, H/d = 0.5, and Re = 35,000, the \(\it {\text{Nu}}_{{{\text{avg}}}}\) Nu avg , \(\it {\text{Nu}}_{{{\text{avg}}/phantom{i}{\text{.r}}}}\) Nu avg / phantom i .r , and \(\it {\text{PEC}}\) PEC equal 127, 2.45, and 2.88, respectively. As well, DREs significantly reduce the recirculation zone downstream of the roughness elements.