Inverse Design of Cooling Arrays of Micro Pin-Fins Subject to Specified Coolant Inlet Temperature and Hot Spot Temperature
Given a micro pin-fin array cooling scheme with these constraints: (a) given maximum allowable temperature of the material (the hot spot temperature), (b) given inlet cooling fluid temperature, (c) given total pressure loss (pumping power affordable), and (d) given overall thickness of the entire mi...
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Published in | Heat transfer engineering Vol. 38; no. 13; pp. 1147 - 1156 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Philadelphia
Taylor & Francis
02.09.2017
Taylor & Francis Ltd |
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Online Access | Get full text |
ISSN | 0145-7632 1521-0537 |
DOI | 10.1080/01457632.2016.1239924 |
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Abstract | Given a micro pin-fin array cooling scheme with these constraints: (a) given maximum allowable temperature of the material (the hot spot temperature), (b) given inlet cooling fluid temperature, (c) given total pressure loss (pumping power affordable), and (d) given overall thickness of the entire micro pin-fin cooling array, find the maximum possible average heat flux on the hot surface and find the maximum possible heat flux at the hot spot under the condition that the entire amount of the inputted heat is removed by the cooling fluid. The goal was to create an optimum performance map for a cooling micro array having specified inlet coolant temperature and maximum temperature. Fully 3D conjugate heat transfer analysis was performed on each of the randomly created candidate configurations. Response surfaces based on Radial Basis Functions were coupled with a genetic algorithm to arrive at a Pareto set of best trade-off solutions. These Pareto optimized configurations indicate the maximum physically possible heat fluxes for specified material and constraints. Detailed off-design performance maps of such Pareto-optimized cooling arrays of micro pin-fins were calculated that demonstrate superior on-design and off-design performance of pin-fins having symmetric convex cross sections as opposed to the commonly used circular cross sections. |
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AbstractList | Not provided. Given a micro pin-fin array cooling scheme with these constraints: (a) given maximum allowable temperature of the material (the hot spot temperature), (b) given inlet cooling fluid temperature, (c) given total pressure loss (pumping power affordable), and (d) given overall thickness of the entire micro pin-fin cooling array, find the maximum possible average heat flux on the hot surface and find the maximum possible heat flux at the hot spot under the condition that the entire amount of the inputted heat is removed by the cooling fluid. The goal was to create an optimum performance map for a cooling micro array having specified inlet coolant temperature and maximum temperature. Fully 3D conjugate heat transfer analysis was performed on each of the randomly created candidate configurations. Response surfaces based on Radial Basis Functions were coupled with a genetic algorithm to arrive at a Pareto set of best trade-off solutions. These Pareto optimized configurations indicate the maximum physically possible heat fluxes for specified material and constraints. Detailed off-design performance maps of such Pareto-optimized cooling arrays of micro pin-fins were calculated that demonstrate superior on-design and off-design performance of pin-fins having symmetric convex cross sections as opposed to the commonly used circular cross sections. |
Author | Reddy, Sohail R. Dulikravich, George S. |
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BackLink | https://www.osti.gov/biblio/1535371$$D View this record in Osti.gov |
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CitedBy_id | crossref_primary_10_1002_htj_23016 crossref_primary_10_1080_01457632_2019_1637136 crossref_primary_10_1016_j_ijheatmasstransfer_2021_121590 crossref_primary_10_1016_j_ijthermalsci_2018_07_043 crossref_primary_10_1016_j_mfglet_2019_11_005 crossref_primary_10_1016_j_ijheatmasstransfer_2020_119843 crossref_primary_10_1115_1_4066748 crossref_primary_10_1016_j_applthermaleng_2019_114721 crossref_primary_10_1080_10426914_2021_1948051 crossref_primary_10_1080_01457632_2023_2241175 crossref_primary_10_1115_1_4053168 crossref_primary_10_3390_en13071631 |
Cites_doi | 10.1016/j.ijheatfluidflow.2013.10.004 10.1115/1.1924624 10.3390/e3050293 10.1016/j.ijheatmasstransfer.2013.07.039 10.1016/0041-5553(67)90144-9 10.1080/15567260903058033 10.1016/j.ijthermalsci.2014.12.021 10.14741/ijcet/spl.2.2014.88 10.1109/4235.996017 10.1016/j.ijheatmasstransfer.2010.02.021 10.1016/j.ijheatmasstransfer.2012.03.022 |
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Copyright | 2017 Taylor & Francis Group, LLC 2017 2017 Taylor & Francis Group, LLC |
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References | cit0011 John T.J. (cit0005) cit0020 cit0021 Bar-Cohen A. (cit0001); 4 Bejan A. (cit0022) Dennis B. H. (cit0017) Hardy R.L. (cit0019); 176 Prasher R. (cit0012) Reddy S.R. (cit0010) Balakrishna B. (cit0015) Siu-Ho A.M. (cit0004) cit0008 Abdoli A. (cit0003); 37 cit0009 cit0006 AlWaaly A.A. (cit0013) cit0007 cit0018 cit0016 cit0002 Reddy S. (cit0023); 38 |
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SubjectTerms | Arrays Coolants Cooling Engineering Heat Heat flux Heat transfer Hot spots Inlets Inverse design Mechanics Temperature Thermodynamics |
Title | Inverse Design of Cooling Arrays of Micro Pin-Fins Subject to Specified Coolant Inlet Temperature and Hot Spot Temperature |
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