Influence of Narrow Rectangular Channel (AR=1:4) on Heat Transfer and Friction for V- and W-Shaped Ribs in Turbine Blade Applications

Effective cooling of blades with a nominal pressure drop is essential for performance augmentation and thermal management of gas turbines. Hence, present work is aimed at determining the heat transfer enhancement and friction for W- and V-shaped ribs inside a rectangular cooling channel having hydra...

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Main Authors: Karthik Krishnaswamy, Suresh Sivan, Hafiz Muhammad Ali
Format: Article
Language:English
Published: Wiley 2021-01-01
Series:International Journal of Photoenergy
Online Access:http://dx.doi.org/10.1155/2021/5581081
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author Karthik Krishnaswamy
Suresh Sivan
Hafiz Muhammad Ali
author_facet Karthik Krishnaswamy
Suresh Sivan
Hafiz Muhammad Ali
author_sort Karthik Krishnaswamy
collection DOAJ
description Effective cooling of blades with a nominal pressure drop is essential for performance augmentation and thermal management of gas turbines. Hence, present work is aimed at determining the heat transfer enhancement and friction for W- and V-shaped ribs inside a rectangular cooling channel having hydraulic diameter (Dh) of 0.048 m and aspect ratio (AR) 1 : 4. Ribs are fixed facing downstream with angle of attack (α) 45° on opposite walls. Pitch (P) between two successive ribs is 25 mm for both cases. Continuous V- and W-shaped ribs with height to channel hydraulic diameter ratio (e/Dh) 0.052 and 0.0416 and pitch to height ratio (P/e) 10 and 12.5, respectively, have been examined for Reynolds number (Re) range 20000-80000. Heat transfer augmentation achieved at Re 80000 is 1.94 and 1.8 times higher than Re 20000 for V- and W-shaped ribs, respectively. Streamwise and spanwise variations in local Nusselt number ratio are highest for V-shaped ribs, which are estimated to be 31% and 12%. For W-shaped ribs, variations are 17.5% and 3.5%. Nusselt number (Nu) is highest along span length 0.5w for V-shaped ribs due to dominance of apex induced secondary flow. For W-shaped ribs, Nusselt number along the span lengths is found to be nearly same view uniformity in secondary flow. Maximum enhancement (Nu/Nuo) estimated for both the rib shapes is 3.9 at Re 20000. Due to increased rib height, friction losses for V-shaped ribs are higher than W-shaped ribs. Maximum friction loss increment is estimated to be 85% for V-shaped ribs and 42% for W-shaped ribs between Re 20000 and 40000. For both rib shapes, impact of ribs is found to be greatest at Re 40000. Thermohydraulic performance (THP) for W-shaped ribs is superior to V-shaped ribs. Best THP achieved for W- and V-shaped ribs are 3.7 and 3.4 at Re 20000.
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spelling doaj-art-4fa8dd03ea5746878e0c3db1a02fd6ca2025-08-20T02:05:37ZengWileyInternational Journal of Photoenergy1110-662X1687-529X2021-01-01202110.1155/2021/55810815581081Influence of Narrow Rectangular Channel (AR=1:4) on Heat Transfer and Friction for V- and W-Shaped Ribs in Turbine Blade ApplicationsKarthik Krishnaswamy0Suresh Sivan1Hafiz Muhammad Ali2Mechanical Engineering, National Institute of Technology, Tiruchirappalli 620015, IndiaMechanical Engineering, National Institute of Technology, Tiruchirappalli 620015, IndiaMechanical Engineering, King Fahd University of Petroleum and Minerals, Dhahran 31261, Saudi ArabiaEffective cooling of blades with a nominal pressure drop is essential for performance augmentation and thermal management of gas turbines. Hence, present work is aimed at determining the heat transfer enhancement and friction for W- and V-shaped ribs inside a rectangular cooling channel having hydraulic diameter (Dh) of 0.048 m and aspect ratio (AR) 1 : 4. Ribs are fixed facing downstream with angle of attack (α) 45° on opposite walls. Pitch (P) between two successive ribs is 25 mm for both cases. Continuous V- and W-shaped ribs with height to channel hydraulic diameter ratio (e/Dh) 0.052 and 0.0416 and pitch to height ratio (P/e) 10 and 12.5, respectively, have been examined for Reynolds number (Re) range 20000-80000. Heat transfer augmentation achieved at Re 80000 is 1.94 and 1.8 times higher than Re 20000 for V- and W-shaped ribs, respectively. Streamwise and spanwise variations in local Nusselt number ratio are highest for V-shaped ribs, which are estimated to be 31% and 12%. For W-shaped ribs, variations are 17.5% and 3.5%. Nusselt number (Nu) is highest along span length 0.5w for V-shaped ribs due to dominance of apex induced secondary flow. For W-shaped ribs, Nusselt number along the span lengths is found to be nearly same view uniformity in secondary flow. Maximum enhancement (Nu/Nuo) estimated for both the rib shapes is 3.9 at Re 20000. Due to increased rib height, friction losses for V-shaped ribs are higher than W-shaped ribs. Maximum friction loss increment is estimated to be 85% for V-shaped ribs and 42% for W-shaped ribs between Re 20000 and 40000. For both rib shapes, impact of ribs is found to be greatest at Re 40000. Thermohydraulic performance (THP) for W-shaped ribs is superior to V-shaped ribs. Best THP achieved for W- and V-shaped ribs are 3.7 and 3.4 at Re 20000.http://dx.doi.org/10.1155/2021/5581081
spellingShingle Karthik Krishnaswamy
Suresh Sivan
Hafiz Muhammad Ali
Influence of Narrow Rectangular Channel (AR=1:4) on Heat Transfer and Friction for V- and W-Shaped Ribs in Turbine Blade Applications
International Journal of Photoenergy
title Influence of Narrow Rectangular Channel (AR=1:4) on Heat Transfer and Friction for V- and W-Shaped Ribs in Turbine Blade Applications
title_full Influence of Narrow Rectangular Channel (AR=1:4) on Heat Transfer and Friction for V- and W-Shaped Ribs in Turbine Blade Applications
title_fullStr Influence of Narrow Rectangular Channel (AR=1:4) on Heat Transfer and Friction for V- and W-Shaped Ribs in Turbine Blade Applications
title_full_unstemmed Influence of Narrow Rectangular Channel (AR=1:4) on Heat Transfer and Friction for V- and W-Shaped Ribs in Turbine Blade Applications
title_short Influence of Narrow Rectangular Channel (AR=1:4) on Heat Transfer and Friction for V- and W-Shaped Ribs in Turbine Blade Applications
title_sort influence of narrow rectangular channel ar 1 4 on heat transfer and friction for v and w shaped ribs in turbine blade applications
url http://dx.doi.org/10.1155/2021/5581081
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