2019
DOI: 10.3390/aerospace6040048
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Investigation of the Trailing Edge Modification Effect on Compressor Blade Aerodynamics Using SST k-ω Turbulence Model

Abstract: A gas turbine power plant in Thailand had the problem of compressor blade fracture in Stages 6–8, 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 solution and outcomes. Three-dimensional (3D) compressor blade models in the problematic stages were prepared by a 3D scanning machine to find a solution based on computational fluid dynamics (CFD), and then were completed for simul… Show more

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Cited by 17 publications
(17 citation statements)
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“…Both models had 2 circular outlets with radius of 10 mm located at a depth of 36.65 mm from the tank edge. The water in the pipe prior to entering inlet and outlet was designed to have a length of 3 cm to prevent it from backflowing and for faster convergence calculations [29]. We modelled that the particles that we wanted to wash were spherical in shape, were Cr 2 O 3 particles, and have a radius of 5 µm.…”
Section: Cfd Settingmentioning
confidence: 99%
“…Both models had 2 circular outlets with radius of 10 mm located at a depth of 36.65 mm from the tank edge. The water in the pipe prior to entering inlet and outlet was designed to have a length of 3 cm to prevent it from backflowing and for faster convergence calculations [29]. We modelled that the particles that we wanted to wash were spherical in shape, were Cr 2 O 3 particles, and have a radius of 5 µm.…”
Section: Cfd Settingmentioning
confidence: 99%
“…Convergent criterion was set as 10 -4 . The turbulence model was shear stress relevant to industrial and medical applications [10][11]. This turbulence model combined the advantages of both k − ω and k − ε turbulence models together, thus enabling us to simulate the fluid's flow behavior in the inner area of the boundary layer accurately, which is the k − ω's uniqueness.…”
Section: Boundary Conditionsmentioning
confidence: 99%
“…The SST k − ω model was shown to have higher accuracy than a common k − ε model. An example of successful usage of the SST k − ω to simulate the airflow in a small volume jet nebulizer was reported in [12] and aerodynamics of trailing blade in a gas turbine was reported in [13]. The SST k −ω model consists of two equations as in Eqs.…”
Section: Governing Equationsmentioning
confidence: 99%
“…Full forms and descriptions of related parameters in Eqs. (1)-(5) can be found in [11,13]. The airflow behavior is derived from the Eqs.…”
Section: Governing Equationsmentioning
confidence: 99%
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