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• W4294031851 abstract "In this paper, measurements of the stall of a NACA [Formula: see text] airfoil section are presented and compared to a simulation with a hybrid Reynolds-averaged Navier–Stokes (RANS)/large-eddy simulation (LES) model with the goal of gaining deeper insight into the flow physics of a stall cell and the turbulent wake in such conditions. Detailed measurements of the evolution of the velocity deficit and turbulence within the wake along with surface pressure measurements and flow visualization provided a comprehensive database for code validation and flow physics studies. The measurements in the Laminar Wind Tunnel of the Institute of Aerodynamics and Gas Dynamics were performed at a Reynolds number of [Formula: see text] and comprised surface pressures, oil flow surface visualizations, and hot-wire measurements of the wake. The results at [Formula: see text] were used as validation data for a hybrid RANS/LES run at the same flow conditions. It was shown that the Bernoulli-based detached eddy simulation (BDES) model, which uses a shielding function based on a localized Bernoulli formulation, combined with effective gray area mitigation can capture the stall cell pattern and the point of flow separation at an angle of attack of [Formula: see text]. Furthermore, the velocity deficit and the Reynolds stresses in the wake show good agreement between simulation and experiment under these conditions." @default.
• W4294031851 created "2022-09-01" @default.
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• W4294031851 date "2022-12-01" @default.
• W4294031851 modified "2023-10-18" @default.
• W4294031851 title "Experimental and Numerical Investigation of Stall on the NACA 64(3) – 418 Airfoil" @default.
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• W4294031851 doi "https://doi.org/10.2514/1.j061922" @default.
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