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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Bibliographic Details
Main Authors: S. Sadasivan, S. K. Arumugam, M. C Aggarwal
Format: Article
Language:English
Published: Isfahan University of Technology 2019-01-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Online Access:http://jafmonline.net/JournalArchive/download?file_ID=47811&issue_ID=253