Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine

A change in combustion concepts from conventional isobaric to constant volume combustion (CVC) has several advantages. Pulse detonation combustion (PDC) operates on CVC, increasing the engine's thermodynamic efficiency significantly. Little research has been conducted on pollutant emissions fro...

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Main Authors: Warimani, Mahammadsalman, Mahaboobali, Fharukh Ahmed Ghasi, Khan, Sher Afghan, Muthuswamy, Sonachalam, Bellary, Sayed Ahmed Imran
Format: Article
Language:English
English
Published: Semarak Ilmu Publishing 2024
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Online Access:http://irep.iium.edu.my/111173/1/111173_Numerical%20investigation%20of%20NOx.pdf
http://irep.iium.edu.my/111173/2/111173_Numerical%20investigation%20of%20NOx_Scopus.pdf
http://irep.iium.edu.my/111173/
https://semarakilmu.com.my/journals/index.php/fluid_mechanics_thermal_sciences/article/view/5984
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Institution: Universiti Islam Antarabangsa Malaysia
Language: English
English
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spelling my.iium.irep.1111732024-05-15T01:06:00Z http://irep.iium.edu.my/111173/ Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine Warimani, Mahammadsalman Mahaboobali, Fharukh Ahmed Ghasi Khan, Sher Afghan Muthuswamy, Sonachalam Bellary, Sayed Ahmed Imran TL1 Motor vehicles A change in combustion concepts from conventional isobaric to constant volume combustion (CVC) has several advantages. Pulse detonation combustion (PDC) operates on CVC, increasing the engine's thermodynamic efficiency significantly. Little research has been conducted on pollutant emissions from pulse detonation engines (PDE). Because PDE burns at a higher temperature, it emits more NOx. The formation of NOx is investigated in this paper using the computational fluid dynamics (CFD) method. For hydrogen fuel, a model is built by varying pressure, temperature, spark size, and geometry. The SST K- Omega model is used with transient conditions. EINOx was calculated using CFD analysis for 12 cm and 20 cm tubes. The results were encouraging. A 12 cm tube produced 200 g/kg of fuel EINOx, while a 20 cm tube produced 250 g/kg of fuel EINOx. The computed results are consistent with previous literature. Semarak Ilmu Publishing 2024-03-03 Article PeerReviewed application/pdf en http://irep.iium.edu.my/111173/1/111173_Numerical%20investigation%20of%20NOx.pdf application/pdf en http://irep.iium.edu.my/111173/2/111173_Numerical%20investigation%20of%20NOx_Scopus.pdf Warimani, Mahammadsalman and Mahaboobali, Fharukh Ahmed Ghasi and Khan, Sher Afghan and Muthuswamy, Sonachalam and Bellary, Sayed Ahmed Imran (2024) Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 114 (2). pp. 106-117. E-ISSN 2289-7879 https://semarakilmu.com.my/journals/index.php/fluid_mechanics_thermal_sciences/article/view/5984 10.37934/arfmts.114.2.106117
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TL1 Motor vehicles
spellingShingle TL1 Motor vehicles
Warimani, Mahammadsalman
Mahaboobali, Fharukh Ahmed Ghasi
Khan, Sher Afghan
Muthuswamy, Sonachalam
Bellary, Sayed Ahmed Imran
Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine
description A change in combustion concepts from conventional isobaric to constant volume combustion (CVC) has several advantages. Pulse detonation combustion (PDC) operates on CVC, increasing the engine's thermodynamic efficiency significantly. Little research has been conducted on pollutant emissions from pulse detonation engines (PDE). Because PDE burns at a higher temperature, it emits more NOx. The formation of NOx is investigated in this paper using the computational fluid dynamics (CFD) method. For hydrogen fuel, a model is built by varying pressure, temperature, spark size, and geometry. The SST K- Omega model is used with transient conditions. EINOx was calculated using CFD analysis for 12 cm and 20 cm tubes. The results were encouraging. A 12 cm tube produced 200 g/kg of fuel EINOx, while a 20 cm tube produced 250 g/kg of fuel EINOx. The computed results are consistent with previous literature.
format Article
author Warimani, Mahammadsalman
Mahaboobali, Fharukh Ahmed Ghasi
Khan, Sher Afghan
Muthuswamy, Sonachalam
Bellary, Sayed Ahmed Imran
author_facet Warimani, Mahammadsalman
Mahaboobali, Fharukh Ahmed Ghasi
Khan, Sher Afghan
Muthuswamy, Sonachalam
Bellary, Sayed Ahmed Imran
author_sort Warimani, Mahammadsalman
title Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine
title_short Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine
title_full Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine
title_fullStr Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine
title_full_unstemmed Numerical investigation of NOx reduction in a hydrogen-fueled pulse detonation engine
title_sort numerical investigation of nox reduction in a hydrogen-fueled pulse detonation engine
publisher Semarak Ilmu Publishing
publishDate 2024
url http://irep.iium.edu.my/111173/1/111173_Numerical%20investigation%20of%20NOx.pdf
http://irep.iium.edu.my/111173/2/111173_Numerical%20investigation%20of%20NOx_Scopus.pdf
http://irep.iium.edu.my/111173/
https://semarakilmu.com.my/journals/index.php/fluid_mechanics_thermal_sciences/article/view/5984
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