This study comprehensively illustrates the effect of Reynolds number, hole spacing, jet-to-target distance and hole inclination on the convective heat transfer performance of an impinging jet array. Highly resolved heat transfer coefficient distributions on the target plate are obtained utilizing transient liquid crystal over a range of Reynolds numbers varying between 5,000 and 25,000. Effect of streamwise and spanwise jet-to-jet spacing (X/D, Y/D: 4–8) and jet-to-target plate distance (Z/D: 0.75–3) are employed composing a test matrix of 36 different geometries. Additionally, the effect of hole inclination (θ: 0°–40°) on the heat transfer coefficient is investigated. Optical hole spacing arrangements and impingement distance are pointed out to maximize the area-averaged Nusselt number and minimize the amount of cooling air. Also included is a new correlation, based on that of Florschuetz et al., to predict row-averaged Nusselt number. The new correlation is capable to cover low Z/D∼0.75 and presents better prediction of row-averaged Nusselt number, which proves to be an effective impingement design tool.
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ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
June 13–17, 2016
Seoul, South Korea
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4979-8
PROCEEDINGS PAPER
Effect of Reynolds Number, Hole Patterns and Hole Inclination on Cooling Performance of an Impinging Jet Array: Part I — Convective Heat Transfer Results and Optimization
Weihong Li,
Weihong Li
Tsinghua University, Beijing, China
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Xueying Li,
Xueying Li
Tsinghua University, Beijing, China
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Hongde Jiang,
Hongde Jiang
Tsinghua University, Beijing, China
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Phillip Ligrani
Phillip Ligrani
University of Alabama in Huntsville, Huntsville, AL
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Weihong Li
Tsinghua University, Beijing, China
Xueying Li
Tsinghua University, Beijing, China
Jing Ren
Tsinghua University, Beijing, China
Hongde Jiang
Tsinghua University, Beijing, China
Li Yang
University of Pittsburgh, Pittsburgh, PA
Phillip Ligrani
University of Alabama in Huntsville, Huntsville, AL
Paper No:
GT2016-56205, V05BT16A003; 13 pages
Published Online:
September 20, 2016
Citation
Li, W, Li, X, Ren, J, Jiang, H, Yang, L, & Ligrani, P. "Effect of Reynolds Number, Hole Patterns and Hole Inclination on Cooling Performance of an Impinging Jet Array: Part I — Convective Heat Transfer Results and Optimization." Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. Volume 5B: Heat Transfer. Seoul, South Korea. June 13–17, 2016. V05BT16A003. ASME. https://doi.org/10.1115/GT2016-56205
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