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Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris

This study presents the validation of two equation turbulence model (k-epsilon) that incorporates fixed variables of exit Reynolds number 2.8 x 106 and 0.79 as exit isentropic Mach number on a turbine blade simulation by ANSYS software. The boundary condition of this study has been set to be 140kPa...

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Main Author: Idris, Nurfazliawati
Format: Thesis
Language:English
Published: 2019
Online Access:https://ir.uitm.edu.my/id/eprint/89197/1/89197.pdf
https://ir.uitm.edu.my/id/eprint/89197/
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spelling my.uitm.ir.891972024-08-15T08:30:00Z https://ir.uitm.edu.my/id/eprint/89197/ Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris Idris, Nurfazliawati This study presents the validation of two equation turbulence model (k-epsilon) that incorporates fixed variables of exit Reynolds number 2.8 x 106 and 0.79 as exit isentropic Mach number on a turbine blade simulation by ANSYS software. The boundary condition of this study has been set to be 140kPa and 280K as the inlet pressure and inlet temperature of the model. The validation of dimensionless pressure distribution, isentropic Mach number and Fast Fourier Transformation (FFT) has been used as parameter study. The result of isentropic Mach number around the blade has recently indicates very good agreement with the experiment while the result of FFT captures the pressure fluctuation at trailing edge of the turbine blade with the 4.6% of discrepancy with experiment result. For the dimensionless pressure distribution, the result has some discrepancy. Then, a new hybrid turbulence model has been done and the improvement of the result has been achieved. The result of hybrid equation shows that isentropic Mach number and dimensionless pressure distribution validation became closer to the experimental result compared to the unmodified equation. Thus, the calculation that should be used to obtain a better result is by isentropic relation for total inlet pressure as it could be farther result to the experiment if directly uses a total pressure. 2019 Thesis NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/89197/1/89197.pdf Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris. (2019) Masters thesis, thesis, Universiti Teknologi MARA (UiTM). <http://terminalib.uitm.edu.my/89197.pdf>
institution Universiti Teknologi Mara
building Tun Abdul Razak Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Mara
content_source UiTM Institutional Repository
url_provider http://ir.uitm.edu.my/
language English
description This study presents the validation of two equation turbulence model (k-epsilon) that incorporates fixed variables of exit Reynolds number 2.8 x 106 and 0.79 as exit isentropic Mach number on a turbine blade simulation by ANSYS software. The boundary condition of this study has been set to be 140kPa and 280K as the inlet pressure and inlet temperature of the model. The validation of dimensionless pressure distribution, isentropic Mach number and Fast Fourier Transformation (FFT) has been used as parameter study. The result of isentropic Mach number around the blade has recently indicates very good agreement with the experiment while the result of FFT captures the pressure fluctuation at trailing edge of the turbine blade with the 4.6% of discrepancy with experiment result. For the dimensionless pressure distribution, the result has some discrepancy. Then, a new hybrid turbulence model has been done and the improvement of the result has been achieved. The result of hybrid equation shows that isentropic Mach number and dimensionless pressure distribution validation became closer to the experimental result compared to the unmodified equation. Thus, the calculation that should be used to obtain a better result is by isentropic relation for total inlet pressure as it could be farther result to the experiment if directly uses a total pressure.
format Thesis
author Idris, Nurfazliawati
spellingShingle Idris, Nurfazliawati
Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris
author_facet Idris, Nurfazliawati
author_sort Idris, Nurfazliawati
title Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris
title_short Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris
title_full Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris
title_fullStr Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris
title_full_unstemmed Numerical simulation for high subsonic turbine blades by modified k-e turbulent models / Nurfazliawati Idris
title_sort numerical simulation for high subsonic turbine blades by modified k-e turbulent models / nurfazliawati idris
publishDate 2019
url https://ir.uitm.edu.my/id/eprint/89197/1/89197.pdf
https://ir.uitm.edu.my/id/eprint/89197/
_version_ 1808975936029196288
score 13.211869

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