Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZ
This study investigates the potential of Yttria-Stabilized Zirconia (YSZ) and Partially Stabilized Zirconia (PSZ) thermal barrier coatings (TBCs) in improving gas turbine performance through a theoretical simulation. Using the finite element method, we compared temperature and thermal flow distribut...
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| Format: | Article |
| Language: | English |
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IOP Publishing
2025-01-01
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| Series: | Materials Research Express |
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| Online Access: | https://doi.org/10.1088/2053-1591/ada874 |
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| author | S M Taseen Wahid Rashidun Nessa Chowdhury Jurana Monjur Muammer Din Arif |
| author_facet | S M Taseen Wahid Rashidun Nessa Chowdhury Jurana Monjur Muammer Din Arif |
| author_sort | S M Taseen Wahid |
| collection | DOAJ |
| description | This study investigates the potential of Yttria-Stabilized Zirconia (YSZ) and Partially Stabilized Zirconia (PSZ) thermal barrier coatings (TBCs) in improving gas turbine performance through a theoretical simulation. Using the finite element method, we compared temperature and thermal flow distributions within YSZ and PSZ coated combustion chambers against an uncoated Ni substrate liner wall. Our results demonstrate significant reductions in outer wall temperature (2.61%–3.54%) and heat flux (0.44%–0.6%) achieved through TBC application. The findings were validated through similar studies, with results aligning closely with established data. These reductions translate to cooler and more efficient engine operation. This comparative analysis not only sheds light on TBC effectiveness but also provides valuable insights for optimizing combustion chamber design. These findings pave the way for the development of next-generation TBC materials and engineering strategies, ultimately leading to enhanced gas turbine performance. |
| format | Article |
| id | doaj-art-941425432e064c359ba20e4b0663820a |
| institution | Kabale University |
| issn | 2053-1591 |
| language | English |
| publishDate | 2025-01-01 |
| publisher | IOP Publishing |
| record_format | Article |
| series | Materials Research Express |
| spelling | doaj-art-941425432e064c359ba20e4b0663820a2025-01-22T19:39:35ZengIOP PublishingMaterials Research Express2053-15912025-01-0112101651210.1088/2053-1591/ada874Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZS M Taseen Wahid0https://orcid.org/0009-0001-2517-3587Rashidun Nessa Chowdhury1https://orcid.org/0009-0004-2875-2885Jurana Monjur2Muammer Din Arif3Department of Mechanical Engineering, Military Institute of science and Technology , Dhaka, 1000, BangladeshDepartment of Mechanical Engineering, Military Institute of science and Technology , Dhaka, 1000, BangladeshDepartment of Mechanical Engineering, Military Institute of science and Technology , Dhaka, 1000, BangladeshDepartment of Mechanical Engineering, Military Institute of science and Technology , Dhaka, 1000, BangladeshThis study investigates the potential of Yttria-Stabilized Zirconia (YSZ) and Partially Stabilized Zirconia (PSZ) thermal barrier coatings (TBCs) in improving gas turbine performance through a theoretical simulation. Using the finite element method, we compared temperature and thermal flow distributions within YSZ and PSZ coated combustion chambers against an uncoated Ni substrate liner wall. Our results demonstrate significant reductions in outer wall temperature (2.61%–3.54%) and heat flux (0.44%–0.6%) achieved through TBC application. The findings were validated through similar studies, with results aligning closely with established data. These reductions translate to cooler and more efficient engine operation. This comparative analysis not only sheds light on TBC effectiveness but also provides valuable insights for optimizing combustion chamber design. These findings pave the way for the development of next-generation TBC materials and engineering strategies, ultimately leading to enhanced gas turbine performance.https://doi.org/10.1088/2053-1591/ada874TBCYSZPSZNiCrAlYcombustion chamber linerFEM |
| spellingShingle | S M Taseen Wahid Rashidun Nessa Chowdhury Jurana Monjur Muammer Din Arif Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZ Materials Research Express TBC YSZ PSZ NiCrAlY combustion chamber liner FEM |
| title | Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZ |
| title_full | Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZ |
| title_fullStr | Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZ |
| title_full_unstemmed | Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZ |
| title_short | Numerical simulation of thermal barrier coating in gas turbine combustion chamber liner: a comparative study of YSZ and PSZ |
| title_sort | numerical simulation of thermal barrier coating in gas turbine combustion chamber liner a comparative study of ysz and psz |
| topic | TBC YSZ PSZ NiCrAlY combustion chamber liner FEM |
| url | https://doi.org/10.1088/2053-1591/ada874 |
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