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...
محفوظ في:
المؤلف الرئيسي: | |
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مؤلفون آخرون: | |
التنسيق: | Theses and Dissertations |
اللغة: | English |
منشور في: |
2009
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الموضوعات: | |
الوصول للمادة أونلاين: | http://hdl.handle.net/10356/19830 |
الوسوم: |
إضافة وسم
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المؤسسة: | Nanyang Technological University |
اللغة: | English |
الملخص: | 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. |
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