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

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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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Mack Breazeale Ph.D.,Michael McPherson 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, turbo

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Mack A. Breazeale,Michael McPhersoned 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 th

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Sound Propagation in the Atmospherenumerical 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

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https://doi.org/10.1007/978-3-030-52171-4 However, coal is considered an environmentally harmful fuel that releases large amounts of greenhouse gases and pollutants during firing. Measures must therefore be taken to improve Pulverized Coal Combustion (PCC) and reduce emissions. Numerical simulations have become increasingly important for t

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https://doi.org/10.1007/978-0-387-26308-3.6, both based on isentropic exit conditions, using a high order discontinuous Galerkin method. The aim is to validate the numerical setup with respect to available experimental data. We discuss the steps taken to create realistic inflow boundary conditions in terms of end wall boundary layer thickn

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