Numerical Simulation of Diffuser of a Gas Turbine using the Actuator Disc Model
An analysis of the exhaust diffuser section of a gas turbine is presented by incorporating the reduced order mathematical model “actuator disc concept” that represents the last stage of the turbine. The actuator disc model is one of the simplified numerical methods for analyzing the aerodynamic perf...
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| Autori principali: | , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
Isfahan University of Technology
2019-01-01
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| Serie: | Journal of Applied Fluid Mechanics |
| Soggetti: | |
| Accesso online: | http://jafmonline.net/JournalArchive/download?file_ID=47811&issue_ID=253 |
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