Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling
f dimple configurations on heat transfer. Specifically, it focuses on the 3x3 array of jets directed at a dimpled target surface. The study explores various jet pitches (P = 3Dj, 4Dj and 5Dj) and distances between jets and the dimpled surface (H = 3Dj, 4Dj and 5Dj). Additionally, dimple designs w...
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Aeronautical and Astronautical Society of the Republic of China
2024
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my.iium.irep.1113792024-03-25T07:27:04Z http://irep.iium.edu.my/111379/ Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling Mohd Zulkeple, Muhammad Fitri Abu Talib, Abd Rahim Harmin, Mohammad Yazdi Saadon, Syamimi Azami, Muhammad Hanafi Yusaf, Talal TJ266 Turbines. Turbomachines (General) f dimple configurations on heat transfer. Specifically, it focuses on the 3x3 array of jets directed at a dimpled target surface. The study explores various jet pitches (P = 3Dj, 4Dj and 5Dj) and distances between jets and the dimpled surface (H = 3Dj, 4Dj and 5Dj). Additionally, dimple designs were altered while keeping their volume constant, resulting in elongated dimples. This investigation comprehensively examines flow patterns and heat transfer properties across Reynolds number (Re) range of 5,000 to 15,000. Increasing the H/Dj ratio from 4 to 5 enlarges entrainment vortices near the target surface due to reduced cross flow intensity between adjacent jets. Conversely, reducing the ratio to 3 intensifies crossflow, delaying cooling jet detachment and enhancing heat transfer. Evaluating the smallest jet-to-jet pitch (Px = 3Dj) reveals enhanced heat transfer to the target surface, driven by increased coolant mass flow rate per unit area compared to larger jet pitches (Px = 4Dj and Px = 5Dj). When altering dimple depths while maintaining constant volume, Nusselt numbers (Nu) showed improvements ranging from 10% to 16%, surpassing the 6% to 14% increase seen with hemisphere dimples Aeronautical and Astronautical Society of the Republic of China 2024-03-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/111379/2/111379_Numerical%20investigation%20of%20heat%20transfer%20enhancement.pdf application/pdf en http://irep.iium.edu.my/111379/8/111379_%20Numerical%20investigation%20of%20heat%20transfer%20enhancement_Scopus.pdf Mohd Zulkeple, Muhammad Fitri and Abu Talib, Abd Rahim and Harmin, Mohammad Yazdi and Saadon, Syamimi and Azami, Muhammad Hanafi and Yusaf, Talal (2024) Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling. Journal of Aeronautics, Astronautics and Aviation, 56 (1S). pp. 93-106. ISSN 1990-7710 https://www.ipress.tw/J0039?pWebID=588&pType=4&mSeq=1 https://doi.org/10.6125/JoAAA.202403_56(1S).02 |
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TJ266 Turbines. Turbomachines (General) Mohd Zulkeple, Muhammad Fitri Abu Talib, Abd Rahim Harmin, Mohammad Yazdi Saadon, Syamimi Azami, Muhammad Hanafi Yusaf, Talal Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling |
description |
f dimple configurations on heat transfer. Specifically, it focuses on the 3x3
array of jets directed at a dimpled target surface. The study explores various
jet pitches (P = 3Dj, 4Dj and 5Dj) and distances between jets and the dimpled
surface (H = 3Dj, 4Dj and 5Dj). Additionally, dimple designs were altered
while keeping their volume constant, resulting in elongated dimples. This
investigation comprehensively examines flow patterns and heat transfer
properties across Reynolds number (Re) range of 5,000 to 15,000. Increasing
the H/Dj ratio from 4 to 5 enlarges entrainment vortices near the target surface
due to reduced cross flow intensity between adjacent jets. Conversely,
reducing the ratio to 3 intensifies crossflow, delaying cooling jet detachment
and enhancing heat transfer. Evaluating the smallest jet-to-jet pitch (Px = 3Dj)
reveals enhanced heat transfer to the target surface, driven by increased
coolant mass flow rate per unit area compared to larger jet pitches (Px = 4Dj
and Px = 5Dj). When altering dimple depths while maintaining constant
volume, Nusselt numbers (Nu) showed improvements ranging from 10% to
16%, surpassing the 6% to 14% increase seen with hemisphere dimples |
format |
Article |
author |
Mohd Zulkeple, Muhammad Fitri Abu Talib, Abd Rahim Harmin, Mohammad Yazdi Saadon, Syamimi Azami, Muhammad Hanafi Yusaf, Talal |
author_facet |
Mohd Zulkeple, Muhammad Fitri Abu Talib, Abd Rahim Harmin, Mohammad Yazdi Saadon, Syamimi Azami, Muhammad Hanafi Yusaf, Talal |
author_sort |
Mohd Zulkeple, Muhammad Fitri |
title |
Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling |
title_short |
Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling |
title_full |
Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling |
title_fullStr |
Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling |
title_full_unstemmed |
Numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling |
title_sort |
numerical investigation of heat transfer enhancement via dimpled target surface configuration and jet arrangement in impingement cooling |
publisher |
Aeronautical and Astronautical Society of the Republic of China |
publishDate |
2024 |
url |
http://irep.iium.edu.my/111379/2/111379_Numerical%20investigation%20of%20heat%20transfer%20enhancement.pdf http://irep.iium.edu.my/111379/8/111379_%20Numerical%20investigation%20of%20heat%20transfer%20enhancement_Scopus.pdf http://irep.iium.edu.my/111379/ https://www.ipress.tw/J0039?pWebID=588&pType=4&mSeq=1 https://doi.org/10.6125/JoAAA.202403_56(1S).02 |
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