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Titlebook: Direct and Large-Eddy Simulation IV; Bernard J. Geurts,Rainer Friedrich,Olivier Métais Book 2001 Springer Science+Business Media Dordrecht

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Springer Handbook of Mechanical Engineeringindtunnel experiments. This configuration still constitutes a challenging test case for Reynolds Averaged Navier-Stokes (RANS) simulation and LES due to the complexity of the suction side boundary layer: an adverse pressure gradient creates successively a laminar separation bubble, a turbulent reatt
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1382-4309 AC workshops that originated at the University of Surrey in 1994. Over the years the DLES-series has grown into a major international venue focused on the development and application of direct and large-eddy simulation. Fundamental turbulence - and modeling issues but also elements from modem numeri
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Wolfgang Buck,Steffen Rudtsch Dr. Results for disturbance growth in Poiseuille flow and LES of turbulent channel flow indicate that the scheme is superior to the 6th-order . approximation proposed by Morinishi .. (1998). The extension to non-periodic boundary conditions is demonstrated for a spatially developing turbulent boundary layer.
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Surface and Interface Characterization(./..). for . > ... This resulting forcing induces a very rapid depletion of the energy cascade at wavenumbers . > ... Two-point statistics of a model implementation compare well with corresponding statistics obtained from direct numerical simulations.
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Pressure Vessels and Heat Exchangersextent in order to obtain a satisfactory result. Spanwise shear makes the flow around a cylinder highly complex through the resulting secondary flow. Here, the competition between the spanwise coupling and the spanwise inhomogenity is investigated.
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A Finite-Mode Spectral Model of Homogeneous and Isotropic Navier-Stokes Turbulence,(./..). for . > ... This resulting forcing induces a very rapid depletion of the energy cascade at wavenumbers . > ... Two-point statistics of a model implementation compare well with corresponding statistics obtained from direct numerical simulations.
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Numerical Simulation of Turbulent Reacting Flow,in the streamwise direction is restored by means of a “fringe region”. Results are presented for two cases: A) a non-reactive scalar released from a line source and B) two reactive scalars released from two different line sources.
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Transition in LES of Bluff Body Flows and Airfoils,extent in order to obtain a satisfactory result. Spanwise shear makes the flow around a cylinder highly complex through the resulting secondary flow. Here, the competition between the spanwise coupling and the spanwise inhomogenity is investigated.
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