Stress analysis of a centrifugal compressor for a mini-jet engine

Stress analysis of a centrifugal compressor for a mini-jet engine

This project encompasses a detailed study of components and mechanism of a SR-30 mini-jet engine. The main objective of this project is to understand the working of the centrifugal compressor and investigate the various stresses undergone by its impeller blades. The analysis is done by computational...

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Main Author: Sinha, Arpita
Other Authors: School of Mechanical and Aerospace Engineering
Format: Final Year Project
Language:English
Published: 2012
Subjects:
DRNTU::Engineering::Aeronautical engineering
Online Access:http://hdl.handle.net/10356/50447
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Institution: Nanyang Technological University
Language: English
id sg-ntu-dr.10356-50447
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spelling sg-ntu-dr.10356-504472023-03-04T18:19:58Z Stress analysis of a centrifugal compressor for a mini-jet engine Sinha, Arpita School of Mechanical and Aerospace Engineering Fei Duan DRNTU::Engineering::Aeronautical engineering This project encompasses a detailed study of components and mechanism of a SR-30 mini-jet engine. The main objective of this project is to understand the working of the centrifugal compressor and investigate the various stresses undergone by its impeller blades. The analysis is done by computational simulation using FEA solver. Bachelor of Engineering (Aerospace Engineering) 2012-06-04T08:33:01Z 2012-06-04T08:33:01Z 2012 2012 Final Year Project (FYP) http://hdl.handle.net/10356/50447 en Nanyang Technological University 79 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
Sinha, Arpita
Stress analysis of a centrifugal compressor for a mini-jet engine
description This project encompasses a detailed study of components and mechanism of a SR-30 mini-jet engine. The main objective of this project is to understand the working of the centrifugal compressor and investigate the various stresses undergone by its impeller blades. The analysis is done by computational simulation using FEA solver.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Sinha, Arpita
format Final Year Project
author Sinha, Arpita
author_sort Sinha, Arpita
title Stress analysis of a centrifugal compressor for a mini-jet engine
title_short Stress analysis of a centrifugal compressor for a mini-jet engine
title_full Stress analysis of a centrifugal compressor for a mini-jet engine
title_fullStr Stress analysis of a centrifugal compressor for a mini-jet engine
title_full_unstemmed Stress analysis of a centrifugal compressor for a mini-jet engine
title_sort stress analysis of a centrifugal compressor for a mini-jet engine
publishDate 2012
url http://hdl.handle.net/10356/50447
_version_ 1759854479590555648

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