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- W4283514219 abstract "The main focus of this paper is on the simulation of flow past a three-dimensional wing-body configuration (DLR-F6) in ground effect; a complex 3D wing-body configuration in ground effect has never been analyzed in the aerodynamics literature to date. For the purpose of validation of the simulation approach, computations are performed for the DLR-F6 wing-body in unbounded flow and are compared with the experimental data. The commercial CFD solver ANSYS FLUENT is employed for computations. Compressible Reynolds-Averaged Navier-Stokes (RANS) equations in conjunction with Spalart-Allmaras (SA) and k-ω Shear Stress Transport (SST) turbulence models are solved. The validated code is employed to calculate the flow field in ground effect; the effects of flight heights above the ground on the aerodynamic properties and flow field are analyzed." @default.
- W4283514219 created "2022-06-27" @default.
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- W4283514219 date "2022-09-01" @default.
- W4283514219 modified "2023-09-27" @default.
- W4283514219 title "Numerical simulation of DLR-F6 wing-body flow field in ground effect" @default.
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- W4283514219 doi "https://doi.org/10.1016/j.compfluid.2022.105576" @default.
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