Investigation of the Trailing Edge Modification Effect on Compressor Blade Aerodynamics Using SST <i>k</i>-<i>ω</i> Turbulence Model

Investigation of the Trailing Edge Modification Effect on Compressor Blade Aerodynamics Using SST <i>k</i>-<i>ω</i> Turbulence Model

A gas turbine power plant in Thailand had the problem of compressor blade fracture in Stages 6&#8722;8, which was caused by housing damage. This gas turbine has a total of 15 stages. The housing damage reduced the lifetime of blades to an unacceptable level. This article shall report the solutio...

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Bibliographic Details
Main Authors: Mongkol Kaewbumrung, Worapol Tangsopa, Jatuporn Thongsri
Format: Article
Language:English
Published: MDPI AG 2019-04-01
Series:Aerospace
Subjects:
ANSYS CFX software
compressor blade
computational fluid dynamics
gas turbine
power plant
simulation
SST <i>k</i>-<i>ω</i> turbulence model
trailing edge
Online Access:https://www.mdpi.com/2226-4310/6/4/48

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https://www.mdpi.com/2226-4310/6/4/48

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