2005
DOI: 10.1590/s1678-58782005000300011
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A source wake model for cascades of axial flow turbomachines

Abstract: This work presents a computational model for the viscous flow through

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Cited by 4 publications
(2 citation statements)
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“…On the other hand, numerical solutions with low computational cost, such as the methods of contour elements and the method of panels with nonviscous viscous interaction, are appropriate to integrate with evolutionary optimization algorithms considering two-dimensional solutions. [50][51][52] Muratoglu and Yuce 53 introduced a study using the integration of CFD and optimization algorithms, considering a constant velocity flow applied to a riverine hydrokinetic turbine regulated by stalls. The study of optimization of the rotor blades was carried out by means of a genetic algorithm using the SST turbulence model.…”
Section: Cfd Study On Turbomachinerymentioning
confidence: 99%
“…On the other hand, numerical solutions with low computational cost, such as the methods of contour elements and the method of panels with nonviscous viscous interaction, are appropriate to integrate with evolutionary optimization algorithms considering two-dimensional solutions. [50][51][52] Muratoglu and Yuce 53 introduced a study using the integration of CFD and optimization algorithms, considering a constant velocity flow applied to a riverine hydrokinetic turbine regulated by stalls. The study of optimization of the rotor blades was carried out by means of a genetic algorithm using the SST turbulence model.…”
Section: Cfd Study On Turbomachinerymentioning
confidence: 99%
“…An improved version of PM is used by [21,22] for 2D cascade design and flow modeling, in his work only pressure distribution is estimated, whereas [23] used the similar technique to estimate the aeroelastic stability parameters, but in this work only camber surface of the blade is modeled not the actual geometry. Furthermore, Ramierez et al [24] employed a modified version of PM with viscousinviscid coupling technique to study the boundary layer separation and the aerodynamic characteristics in the rectilinear 2D blade cascade. In an other study Chen et al [25] have used a 2D frequency domain source-doublet based PM to estimate the 2D and quasi 3D blade loading in centrifugal type turbomachinery system.…”
mentioning
confidence: 99%