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Wake and aerodynamics loads in multiple bodies—application to turbomachinery blade rows
AbstractTwo-dimensional, unsteady flow around bodies of complex geometry (or multiple bodies) at high Reynolds number is simulated using the vortex method. This method is modified to take into account the sub-grid scale phenomena through a second order velocity structure function model adapted to the Lagrangian scheme. The dynamics of the body wake is computed using the convection–diffusion splitting algorithm; the convection process is carried out with a Lagrangian Adams–Bashforth time-marching scheme and the diffusion process is simulated using the random walk method. The pressure distribution is obtained using an integral equation derived from the pressure Poisson equation, which was first developed for a single body. Results for the numerical simulation around a linear cascade of airfoils are presented. As the flow is periodic in the y direction, the discrete vortex shedding need only be considered for a reference airfoil. The flow characteristics around the NACA 65-410 series airfoils are calculated and comparisons are made with results available in the literature.
Wake and aerodynamics loads in multiple bodies—application to turbomachinery blade rows
AbstractTwo-dimensional, unsteady flow around bodies of complex geometry (or multiple bodies) at high Reynolds number is simulated using the vortex method. This method is modified to take into account the sub-grid scale phenomena through a second order velocity structure function model adapted to the Lagrangian scheme. The dynamics of the body wake is computed using the convection–diffusion splitting algorithm; the convection process is carried out with a Lagrangian Adams–Bashforth time-marching scheme and the diffusion process is simulated using the random walk method. The pressure distribution is obtained using an integral equation derived from the pressure Poisson equation, which was first developed for a single body. Results for the numerical simulation around a linear cascade of airfoils are presented. As the flow is periodic in the y direction, the discrete vortex shedding need only be considered for a reference airfoil. The flow characteristics around the NACA 65-410 series airfoils are calculated and comparisons are made with results available in the literature.
Wake and aerodynamics loads in multiple bodies—application to turbomachinery blade rows
Pereira, Luiz Antonio Alcântara (author) / Hirata, Miguel Hiroo (author) / Filho, Nelson Manzanares (author)
Journal of Wind Engineering and Industrial Aerodynamics ; 92 ; 477-491
2004-02-10
15 pages
Article (Journal)
Electronic Resource
English
Wake and aerodynamics loads in multiple bodies-application to turbomachinery blade rows
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