Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad

The axial-flow compressor consists of a series of stages, each comprising a row of rotor blades followed by a row of stator blades. The working fluid in our thesis regarded as an air is initially accelerated by the rotor blades. Then, this working fluid was decelerated in the stator blades passages....

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Main Authors:	Muhamad, Mohd Najib, Jusoh, Mohd Hazlim
Format:	Student Project
Language:	English
Published:	Faculty of Mechanical Engineering 2003
Subjects:	Gas turbines
Online Access:	http://ir.uitm.edu.my/id/eprint/21148/ http://ir.uitm.edu.my/id/eprint/21148/1/PPd_MOHD%20HAZLIM%20JUSOH%20EM%2003_5.pdf

id	uitm-21148
recordtype	eprints
spelling	uitm-211482018-10-17T05:15:55Z http://ir.uitm.edu.my/id/eprint/21148/ Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad Muhamad, Mohd Najib Jusoh, Mohd Hazlim Gas turbines The axial-flow compressor consists of a series of stages, each comprising a row of rotor blades followed by a row of stator blades. The working fluid in our thesis regarded as an air is initially accelerated by the rotor blades. Then, this working fluid was decelerated in the stator blades passages. The kinetic energy transferred in the rotor is converted to static pressure. The process is repeated in as many stages as are necessary to yield the required overall pressure ratio. However, the process that repeated in as many stages finally make the blades change. The changing that we talk here is not a really big change, but it is a tiny one. The changing that no body care about it. But, because this two characteristics, first it is micro and second no body take note, so this thing become more interesting. The change that we discussing here is the changing that happen at the blade inlet and outlet angle. This thing is happen because the working fluid that go through the compressor finally left the particles onto the blade surface. The existence of this particles make the camber line change, and from that the blade angles are change too. Faculty of Mechanical Engineering 2003 Student Project NonPeerReviewed text en http://ir.uitm.edu.my/id/eprint/21148/1/PPd_MOHD%20HAZLIM%20JUSOH%20EM%2003_5.pdf Muhamad, Mohd Najib and Jusoh, Mohd Hazlim (2003) Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad. [Student Project] (Unpublished)
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Teknologi MARA
building	UiTM Institutional Repository
collection	Online Access
language	English
topic	Gas turbines
spellingShingle	Gas turbines Muhamad, Mohd Najib Jusoh, Mohd Hazlim Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad
description	The axial-flow compressor consists of a series of stages, each comprising a row of rotor blades followed by a row of stator blades. The working fluid in our thesis regarded as an air is initially accelerated by the rotor blades. Then, this working fluid was decelerated in the stator blades passages. The kinetic energy transferred in the rotor is converted to static pressure. The process is repeated in as many stages as are necessary to yield the required overall pressure ratio. However, the process that repeated in as many stages finally make the blades change. The changing that we talk here is not a really big change, but it is a tiny one. The changing that no body care about it. But, because this two characteristics, first it is micro and second no body take note, so this thing become more interesting. The change that we discussing here is the changing that happen at the blade inlet and outlet angle. This thing is happen because the working fluid that go through the compressor finally left the particles onto the blade surface. The existence of this particles make the camber line change, and from that the blade angles are change too.
format	Student Project
author	Muhamad, Mohd Najib Jusoh, Mohd Hazlim
author_facet	Muhamad, Mohd Najib Jusoh, Mohd Hazlim
author_sort	Muhamad, Mohd Najib
title	Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad
title_short	Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad
title_full	Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad
title_fullStr	Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad
title_full_unstemmed	Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad
title_sort	performance analysis of a fouled axial-flow compressor blades of a gas turbine / mohd hazlim jusoh and mohd najib muhamad
publisher	Faculty of Mechanical Engineering
publishDate	2003
url	http://ir.uitm.edu.my/id/eprint/21148/ http://ir.uitm.edu.my/id/eprint/21148/1/PPd_MOHD%20HAZLIM%20JUSOH%20EM%2003_5.pdf
first_indexed	2023-09-18T23:05:57Z
last_indexed	2023-09-18T23:05:57Z
_version_	1777418483575816192

Performance analysis of a fouled axial-flow compressor blades of a gas turbine / Mohd Hazlim Jusoh and Mohd Najib Muhamad

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