Design of mini-jet engine turbine wheel

Design of mini-jet engine turbine wheel

The report consists of a detailed study on the axial turbine of mini-jet engines; the basic operation of the turbine; the performance analysis; the flow phenomena and losses in the turbine; the failure mechanism of the turbine. A design software from CONCEPTS NREC is used to investigate the effects...

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Main Author: Koh, Yiyuan.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Industrial Attachment (IA)
Language:English
Published: 2012
Subjects:
DRNTU::Engineering::Aeronautical engineering
Online Access:http://hdl.handle.net/10356/50826
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Institution: Nanyang Technological University
Language: English
id sg-ntu-dr.10356-50826
record_format dspace
spelling sg-ntu-dr.10356-508262023-03-04T18:22:31Z Design of mini-jet engine turbine wheel Koh, Yiyuan. School of Mechanical and Aerospace Engineering Fei Duan DRNTU::Engineering::Aeronautical engineering The report consists of a detailed study on the axial turbine of mini-jet engines; the basic operation of the turbine; the performance analysis; the flow phenomena and losses in the turbine; the failure mechanism of the turbine. A design software from CONCEPTS NREC is used to investigate the effects of various geometric modifications, i.e. blade angles, stagger, aspect ratio, on the performance of the turbine. The report aims to serve as a reference for future re-designing of mini-jet engines. 2012-11-15T08:32:26Z 2012-11-15T08:32:26Z 2011 2011 Industrial Attachment (IA) http://hdl.handle.net/10356/50826 en Nanyang Technological University 121 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering
spellingShingle DRNTU::Engineering::Aeronautical engineering
Koh, Yiyuan.
Design of mini-jet engine turbine wheel
description The report consists of a detailed study on the axial turbine of mini-jet engines; the basic operation of the turbine; the performance analysis; the flow phenomena and losses in the turbine; the failure mechanism of the turbine. A design software from CONCEPTS NREC is used to investigate the effects of various geometric modifications, i.e. blade angles, stagger, aspect ratio, on the performance of the turbine. The report aims to serve as a reference for future re-designing of mini-jet engines.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Koh, Yiyuan.
format Industrial Attachment (IA)
author Koh, Yiyuan.
author_sort Koh, Yiyuan.
title Design of mini-jet engine turbine wheel
title_short Design of mini-jet engine turbine wheel
title_full Design of mini-jet engine turbine wheel
title_fullStr Design of mini-jet engine turbine wheel
title_full_unstemmed Design of mini-jet engine turbine wheel
title_sort design of mini-jet engine turbine wheel
publishDate 2012
url http://hdl.handle.net/10356/50826
_version_ 1759854444804046848

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