Computational Fluid Dynamic Analysis of a Supersonic Turbine
The purpose of this work is to study numerically the flow in a supersonic axial flow impulse turbine. Computations were made with Ansys 15 CFD package, with a 3-dimensional model of one stator-rotor stage. The software implements a “mixing plane model” at the interface between the stator domain, whi...
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| Autores principales: | , |
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| Formato: | Objeto de conferencia Resumen |
| Lenguaje: | Inglés |
| Publicado: |
2015
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| Materias: | |
| Acceso en línea: | http://sedici.unlp.edu.ar/handle/10915/123978 http://congress.cimne.com/PANACM2015/admin/files/fileabstract/a634.pdf |
| Aporte de: |
| Sumario: | The purpose of this work is to study numerically the flow in a supersonic axial flow impulse turbine. Computations were made with Ansys 15 CFD package, with a 3-dimensional model of one stator-rotor stage. The software implements a “mixing plane model” at the interface between the stator domain, which is stationary, and the rotor domain, which is rotating at a prescribed angular velocity, allowing computing each region separately. The flow information between these domains will be coupled at the mixing plane interface. |
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