Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori

The purpose of this research was to determine the performances of the gas turbine aeroengine specifically in design point optimization. The main objective of parametric cycle analysis is to relate the engine performance parameters which are net thrust (FN) and specific fuel consumption (SFC) to desi...

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Main Author:	Wan Sapiansori, Wan Mohd Hafizq
Format:	Thesis
Language:	English
Published:	2009
Subjects:	Machine design and drawing Machine construction (General)
Online Access:	https://ir.uitm.edu.my/id/eprint/38947/1/38947.pdf
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id	my-uitm-ir.38947
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spelling	my-uitm-ir.389472023-07-21T01:40:15Z Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori 2009-11 Wan Sapiansori, Wan Mohd Hafizq Machine design and drawing Machine construction (General) The purpose of this research was to determine the performances of the gas turbine aeroengine specifically in design point optimization. The main objective of parametric cycle analysis is to relate the engine performance parameters which are net thrust (FN) and specific fuel consumption (SFC) to design choices such as compressor pressure ratio (PR), fan pressure ratio (FPR), bypass pressure ratio (BPR), to design limitations such as turbine entry temperature (TET), compressor exit pressure with the flight environment such as Mach number, ambient pressure and temperature. From this analysis, we can easily to determine the engine type, shape and size of engine components to give optimum performance. To develop design point result, MATLAB and SIMULINK software being use to develop computer program for developing the result of all performances with interactive human interface. From research, the set value of output parameter such as thrust and TSFC calculated by the computer software results the variation of input parameter design such as altitude, Mach number and TET and from these data set, the design point of a gas turbine aeroengine type and size can be determine. The significant of the research is to developing computer software for Propulsion Laboratory Faculty of Mechanical Engineering for students to study related field regarding to gas turbine cycle such as thermodynamics and propulsion. 2009-11 Thesis https://ir.uitm.edu.my/id/eprint/38947/ https://ir.uitm.edu.my/id/eprint/38947/1/38947.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering Mohd Noh, Mohd Hafiz
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Mohd Noh, Mohd Hafiz
topic	Machine design and drawing Machine construction (General)
spellingShingle	Machine design and drawing Machine construction (General) Wan Sapiansori, Wan Mohd Hafizq Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori
description	The purpose of this research was to determine the performances of the gas turbine aeroengine specifically in design point optimization. The main objective of parametric cycle analysis is to relate the engine performance parameters which are net thrust (FN) and specific fuel consumption (SFC) to design choices such as compressor pressure ratio (PR), fan pressure ratio (FPR), bypass pressure ratio (BPR), to design limitations such as turbine entry temperature (TET), compressor exit pressure with the flight environment such as Mach number, ambient pressure and temperature. From this analysis, we can easily to determine the engine type, shape and size of engine components to give optimum performance. To develop design point result, MATLAB and SIMULINK software being use to develop computer program for developing the result of all performances with interactive human interface. From research, the set value of output parameter such as thrust and TSFC calculated by the computer software results the variation of input parameter design such as altitude, Mach number and TET and from these data set, the design point of a gas turbine aeroengine type and size can be determine. The significant of the research is to developing computer software for Propulsion Laboratory Faculty of Mechanical Engineering for students to study related field regarding to gas turbine cycle such as thermodynamics and propulsion.
format	Thesis
qualification_level	Bachelor degree
author	Wan Sapiansori, Wan Mohd Hafizq
author_facet	Wan Sapiansori, Wan Mohd Hafizq
author_sort	Wan Sapiansori, Wan Mohd Hafizq
title	Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori
title_short	Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori
title_full	Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori
title_fullStr	Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori
title_full_unstemmed	Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori
title_sort	prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / wan mohd hafizq wan sapiansori
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/38947/1/38947.pdf
_version_	1783734492938108928

Prediction of an aeroengine performance analysis thermodynamic parametric study (design point study) / Wan Mohd Hafizq Wan Sapiansori

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