Numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery
A good understanding of the computational fluid dynamics associated with rotor/stator configurations can be extremely useful when optimising the performance of turbomachinery. In this thesis, a quasi-three-dimensional, implicit, finite volume, time marching Navier-Stokes approach has been used to...
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التنسيق: | Theses and Dissertations |
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sg-ntu-dr.10356-198302023-03-11T17:35:31Z Numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery Miao, Yi. Ng, Yin Kwee School of Mechanical and Production Engineering DRNTU::Engineering::Mechanical engineering::Fluid mechanics A good understanding of the computational fluid dynamics associated with rotor/stator configurations can be extremely useful when optimising the performance of turbomachinery. In this thesis, a quasi-three-dimensional, implicit, finite volume, time marching Navier-Stokes approach has been used to investigate the flow through three cases of the single stage in two subsonic turbines and a transonic compressor. Relative motion between the rotor and stator blades with arbitrary number of airfoils per row is made possible with the use of circumferentially averaging techniques on the inter-row mixing plane. Master of Engineering (MPE) 2009-12-14T06:49:54Z 2009-12-14T06:49:54Z 1996 1996 Thesis http://hdl.handle.net/10356/19830 en NANYANG TECHNOLOGICAL UNIVERSITY 138 p. application/pdf |
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DRNTU::Engineering::Mechanical engineering::Fluid mechanics |
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DRNTU::Engineering::Mechanical engineering::Fluid mechanics Miao, Yi. Numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery |
description |
A good understanding of the computational fluid dynamics associated with rotor/stator
configurations can be extremely useful when optimising the performance of
turbomachinery. In this thesis, a quasi-three-dimensional, implicit, finite volume, time
marching Navier-Stokes approach has been used to investigate the flow through three
cases of the single stage in two subsonic turbines and a transonic compressor. Relative
motion between the rotor and stator blades with arbitrary number of airfoils per row is
made possible with the use of circumferentially averaging techniques on the inter-row
mixing plane. |
author2 |
Ng, Yin Kwee |
author_facet |
Ng, Yin Kwee Miao, Yi. |
format |
Theses and Dissertations |
author |
Miao, Yi. |
author_sort |
Miao, Yi. |
title |
Numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery |
title_short |
Numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery |
title_full |
Numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery |
title_fullStr |
Numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery |
title_full_unstemmed |
Numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery |
title_sort |
numerical investigation of viscous flow through quasi-three dimensional multistage turbomachinery |
publishDate |
2009 |
url |
http://hdl.handle.net/10356/19830 |
_version_ |
1761781755535163392 |