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

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Application of LES to the Thermal–Hydraulics of Target Station 2 of the ISIS Muon and Neutron SourceThe ISIS Muon and Neutron source uses the spallation of protons accelerated to 84 % of the speed of light to generate neutrons at two tungsten targets clad in tantalum and cooled by recirculating water.

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Wind Gust-Induced Flutter of an Elastically Mounted Airfoil: A Fluid-Structure Interaction Study BasClassical investigations on the aeroelasticity of wings used for the analysis of flutter stability are often carried out based on simplifying model configurations given by elastically mounted rigid wings.

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https://doi.org/10.1007/978-3-031-47028-8Fluid Dynamics; Turbulence; Direct Numerical Simulation; Large-Eddy Simulation; LES Modelling; DLES

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978-3-031-47030-1The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl

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Direct and Large Eddy Simulation XIII978-3-031-47028-8Series ISSN 1382-4309 Series E-ISSN 2215-1826

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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, turbomachinery).

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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 the boundary layer, which can lead to stall.