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- W4383889570 abstract "This study numerically analyses the aerodynamic parameters of a base facing triangular cylinder having base length, D in the proximity of a wake splitter plate of Length, L. The gap between the apex of the triangular cylinder and splitter plate is kept as ‘G’. Simulations were done to analyse the effect of G/D and L/D ratios on the coefficient of lift (Cl), drag (CD), and Strouhal number (St). 2-D laminar incompressible flow is analysed at a Reynolds number value of 100, and L/D = 0.5, 1, 1.5, 2.0 at varying gap ratios (G/D) 0 to 4.0. Results indicate that the aerodynamic coefficients are significantly affected by the position of the splitter plate and its length. For L/D ratios 0.5,1.0 and 2, there exists a critical gap ratio at which a sudden jump is observed in the aerodynamic coefficients. Within the parametric space studied, it is also observed that the maximum reduction in Clrms and $$overline{{C}_{d}}$$ is reported at L/D = 2 and G/D = 3.5." @default.
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- W4383889570 date "2023-01-01" @default.
- W4383889570 modified "2023-09-25" @default.
- W4383889570 title "Influence of Wake Splitter Plate on Flow Over a Triangular Cylinder at a Low Reynolds Number: A Numerical Study" @default.
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- W4383889570 doi "https://doi.org/10.1007/978-981-99-2382-3_43" @default.
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