In this study obtaining a uniform heat flux over a target surface was investigated by means of using characteristics of jet impingement heat transfer. Conjugate Gradients Method (CGM) was utilized to minimize the objective function defined on the basis of the squared differences between the target heat flux and the calculated ones. Design variables were taken to be jets’ Reynolds numbers, separation distance between the exit plane of the jets and the target plate, as well as inter-jet spacing. Air single phase jets were used in this study. The problem was solved for the cases of 4 and 6 jets. Temperature difference between the jet exit and the target plate is 100°C, and a steady state condition was assumed. The Finite Volume Method and an unstructured mesh were used for direct solution of the jet impingement heat transfer problem for a laminar jets impingement to a flat plate with constant temperature.
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ASME 2010 10th Biennial Conference on Engineering Systems Design and Analysis
July 12–14, 2010
Istanbul, Turkey
Conference Sponsors:
- International
ISBN:
978-0-7918-4916-3
PROCEEDINGS PAPER
Impinging Jet Cooling Optimization for Obtaining Uniform Heat Flux
Farshad Kowsary,
Farshad Kowsary
University of Tehran, Tehran, Iran
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Hamed Gholamian,
Hamed Gholamian
University of Tehran, Tehran, Iran
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Mehran Rajaeeian Hoonejani
Mehran Rajaeeian Hoonejani
University of California, Santa Barbara, Santa Barbara, CA
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Farshad Kowsary
University of Tehran, Tehran, Iran
Hamed Gholamian
University of Tehran, Tehran, Iran
Mehran Rajaeeian Hoonejani
University of California, Santa Barbara, Santa Barbara, CA
Paper No:
ESDA2010-24362, pp. 525-533; 9 pages
Published Online:
December 28, 2010
Citation
Kowsary, F, Gholamian, H, & Rajaeeian Hoonejani, M. "Impinging Jet Cooling Optimization for Obtaining Uniform Heat Flux." Proceedings of the ASME 2010 10th Biennial Conference on Engineering Systems Design and Analysis. ASME 2010 10th Biennial Conference on Engineering Systems Design and Analysis, Volume 2. Istanbul, Turkey. July 12–14, 2010. pp. 525-533. ASME. https://doi.org/10.1115/ESDA2010-24362
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