CFD analysis of first stage nozzle cooling optimization in power station gas turbine
Computational Fluid Dynamics analysis on First Stage Nozzle in full scale multi-stage power station gas turbine has been carried out. The main aim is to investigate the turbine thermal performance when cooling rate decreases at certain level. All calculations were executed using commercial CFD code,...
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my.uniten.dspace-222462023-05-29T13:59:49Z CFD analysis of first stage nozzle cooling optimization in power station gas turbine Hasini H. Fadhil S.S.A. Jaafar M.N.M. Malek N.A. Ujir M.H. 6507435998 55812738800 57216608088 36994735300 36633279200 Computational Fluid Dynamics analysis on First Stage Nozzle in full scale multi-stage power station gas turbine has been carried out. The main aim is to investigate the turbine thermal performance when cooling rate decreases at certain level. All calculations were executed using commercial CFD code, ANSYS FLUENT which is able to accurately predict the flow and conjugate heat transfer problem as demonstrated in this investigation. The modelling of gas turbine nozzle is assisted by geometric cloud data obtained from 3D scan. Preliminary calculation shows that at the given worst case scenario for, the maximum thermal stress experienced by the component is within the maximum yield strength of the nozzle material. However, the safety margin between the predicted stress and maximum allowable stress is very small. � 2015 Penerbit UTM Press. All rights reserved. Final 2023-05-29T05:59:49Z 2023-05-29T05:59:49Z 2015 Article 10.11113/jt.v76.5540 2-s2.0-84942119114 https://www.scopus.com/inward/record.uri?eid=2-s2.0-84942119114&doi=10.11113%2fjt.v76.5540&partnerID=40&md5=e201fb4ed4a91fde98208de4744155c8 https://irepository.uniten.edu.my/handle/123456789/22246 76 5 73 78 Penerbit UTM Press Scopus |
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Computational Fluid Dynamics analysis on First Stage Nozzle in full scale multi-stage power station gas turbine has been carried out. The main aim is to investigate the turbine thermal performance when cooling rate decreases at certain level. All calculations were executed using commercial CFD code, ANSYS FLUENT which is able to accurately predict the flow and conjugate heat transfer problem as demonstrated in this investigation. The modelling of gas turbine nozzle is assisted by geometric cloud data obtained from 3D scan. Preliminary calculation shows that at the given worst case scenario for, the maximum thermal stress experienced by the component is within the maximum yield strength of the nozzle material. However, the safety margin between the predicted stress and maximum allowable stress is very small. � 2015 Penerbit UTM Press. All rights reserved. |
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6507435998 |
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6507435998 Hasini H. Fadhil S.S.A. Jaafar M.N.M. Malek N.A. Ujir M.H. |
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Hasini H. Fadhil S.S.A. Jaafar M.N.M. Malek N.A. Ujir M.H. |
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Hasini H. Fadhil S.S.A. Jaafar M.N.M. Malek N.A. Ujir M.H. CFD analysis of first stage nozzle cooling optimization in power station gas turbine |
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Hasini H. |
title |
CFD analysis of first stage nozzle cooling optimization in power station gas turbine |
title_short |
CFD analysis of first stage nozzle cooling optimization in power station gas turbine |
title_full |
CFD analysis of first stage nozzle cooling optimization in power station gas turbine |
title_fullStr |
CFD analysis of first stage nozzle cooling optimization in power station gas turbine |
title_full_unstemmed |
CFD analysis of first stage nozzle cooling optimization in power station gas turbine |
title_sort |
cfd analysis of first stage nozzle cooling optimization in power station gas turbine |
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Penerbit UTM Press |
publishDate |
2023 |
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1806423265991720960 |
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13.214268 |