Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance

In this work, an improved counterflow double-channel micro combustor is designed. Computational Fluid Dynamics software Fluent is used to conduct numerical investigations on the thermal performance comparison between the old and improved counterflow double-channel micro combustors. It is found that...

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Main Authors: Zuo, Wei, E, Jiaqiang, Lin, Rongming
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2020
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Online Access:https://hdl.handle.net/10356/144662
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1446622020-11-17T07:42:04Z Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance Zuo, Wei E, Jiaqiang Lin, Rongming School of Mechanical and Aerospace Engineering Engineering::Aeronautical engineering Micro Combustion Counterflow In this work, an improved counterflow double-channel micro combustor is designed. Computational Fluid Dynamics software Fluent is used to conduct numerical investigations on the thermal performance comparison between the old and improved counterflow double-channel micro combustors. It is found that the improved counterflow double-channel micro combustor has much higher and more uniform wall temperature compared that of the old one under various hydrogen mass flow rates, hydrogen/air equivalence ratios and solid materials. To make a quantitative comparison, the main results are presented as follows: (a) The improved combustor achieves the largest thermal enhancement at the hydrogen mass flow rate of 5.25 × 10−7 kg/s when the hydrogen mass flow rate is ranged from 5.25 × 10−7 kg/s to 9.8245 × 10−7 kg/s. Namely, the mean temperature of upper and right wall is improved by about 9.66 K and 13.53 K, respectively, and the mean nonuniformity of upper and right wall temperature is reduced by about 23.24% and 26.79%, respectively. (b) The improved combustor achieves the largest thermal enhancement at the hydrogen/air equivalence ratio of 0.6, when the hydrogen/air equivalence ratio is ranged from 0.9 to 0.5. Namely, the mean temperature of upper and right wall is improved by about 27.55 K and 29.55 K, respectively, and the mean nonuniformity of upper and right wall temperature is reduced by about 23.24% and 19.51%, respectively. (c) The improved combustor achieves the largest thermal enhancement at the solid material of silicon carbide when the solid material is changed from quartz to silicon carbide. Namely, the mean temperature of upper and right wall is improved by about 16.77 K and 18.38 K, respectively, and the mean nonuniformity of upper and right wall temperature is reduced by about 26.47% and 28.41%, respectively. Finally, some guidelines are proposed for applications of the improved counterflow double-channel micro combustor in the micro-thermophotovoltaic system. 2020-11-17T07:42:04Z 2020-11-17T07:42:04Z 2018 Journal Article Zuo, W., E, J., & Lin, R. (2018). Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance. Energy Conversion and Management,159, 163-174. doi:10.1016/j.enconman.2018.01.017 0196-8904 https://hdl.handle.net/10356/144662 10.1016/j.enconman.2018.01.017 159 163 174 en Energy Conversion and Management © 2018 Elsevier Ltd. All rights reserved.
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Aeronautical engineering
Micro Combustion
Counterflow
spellingShingle Engineering::Aeronautical engineering
Micro Combustion
Counterflow
Zuo, Wei
E, Jiaqiang
Lin, Rongming
Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance
description In this work, an improved counterflow double-channel micro combustor is designed. Computational Fluid Dynamics software Fluent is used to conduct numerical investigations on the thermal performance comparison between the old and improved counterflow double-channel micro combustors. It is found that the improved counterflow double-channel micro combustor has much higher and more uniform wall temperature compared that of the old one under various hydrogen mass flow rates, hydrogen/air equivalence ratios and solid materials. To make a quantitative comparison, the main results are presented as follows: (a) The improved combustor achieves the largest thermal enhancement at the hydrogen mass flow rate of 5.25 × 10−7 kg/s when the hydrogen mass flow rate is ranged from 5.25 × 10−7 kg/s to 9.8245 × 10−7 kg/s. Namely, the mean temperature of upper and right wall is improved by about 9.66 K and 13.53 K, respectively, and the mean nonuniformity of upper and right wall temperature is reduced by about 23.24% and 26.79%, respectively. (b) The improved combustor achieves the largest thermal enhancement at the hydrogen/air equivalence ratio of 0.6, when the hydrogen/air equivalence ratio is ranged from 0.9 to 0.5. Namely, the mean temperature of upper and right wall is improved by about 27.55 K and 29.55 K, respectively, and the mean nonuniformity of upper and right wall temperature is reduced by about 23.24% and 19.51%, respectively. (c) The improved combustor achieves the largest thermal enhancement at the solid material of silicon carbide when the solid material is changed from quartz to silicon carbide. Namely, the mean temperature of upper and right wall is improved by about 16.77 K and 18.38 K, respectively, and the mean nonuniformity of upper and right wall temperature is reduced by about 26.47% and 28.41%, respectively. Finally, some guidelines are proposed for applications of the improved counterflow double-channel micro combustor in the micro-thermophotovoltaic system.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Zuo, Wei
E, Jiaqiang
Lin, Rongming
format Article
author Zuo, Wei
E, Jiaqiang
Lin, Rongming
author_sort Zuo, Wei
title Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance
title_short Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance
title_full Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance
title_fullStr Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance
title_full_unstemmed Numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance
title_sort numerical investigations on an improved counterflow double-channel micro combustor fueled with hydrogen for enhancing thermal performance
publishDate 2020
url https://hdl.handle.net/10356/144662
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