Titlebook: Direct and Large Eddy Simulation XIII; Proceedings of DLES1 Cristian Marchioli,Maria Vittoria Salvetti,Philipp Conference proceedings 2024

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Bph773

割公牛膨脹

Large-Eddy Simulations of?the?Accelerating Flow Around a?Square Cylindernterest for wind-engineering applications, typical, e.g., of skyscrapers and towers. Despite the simple geometry, the flow features around square cylinders or prisms show a significant complexity. In particular, the flow is characterized by the shear-layer separation at the upstream edges. The separ

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DNS and?POD Analysis of?Separated Flow in?a?Three-Dimensional Diffusernumerical and experimental data, even without smoothing of the sharp corners. Discrepancies in the duct area have been found to be due to uncertainties, however, in the diffuser region differences are more noticeably between experimental and numerical data, where they all exhibit an oscillating beha

戰(zhàn)役

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Euler-Lagrange LES Predictions of?a?Powder Disperser Including a?Multiscale Wall-Impact Breakage Mode.g., air pollution) and industrial applications (e.g., dry powder inhalers). The main challenge for investigating such flows is the extensive range of length and time scales to be dealt with, especially in the case of turbulent flows.

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Vertebra

Dynamics of?Turbulent Kinetic Energy Advection in?a?Turbulent Boundary Layer Under Unsteady Pressure from the medical field, to engineering applications, to the natural sciences. In most of the practical applications the pressure gradient varies both spatially and temporally giving rise to a transient separation process often associated with a drop in performance of many systems (e.g. wings, turbomachinery).

寵愛

In-Situ Analysis of?Backflow Events and?Their Relation to?Separation in?Wings Through Well-Resolved ed to pressure gradients (PGs). The presence of such PGs affects greatly the development and physics of the turbulent boundary layer (TBL), making it an open research area. An important phenomena associated with the presence of strong adverse PGs (APGs) as appearing in wings, is the separation of the boundary layer, which can lead to stall.