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Advances in Hybrid RANS-LES Modelling Papers contributed to the 2007 Symposium of Hybrid RANS-LES Methods, Corfu, Greece, 17-18 June 2007 /

This volume contains papers contributed to the Second Symposium on Hybrid RANS-LES Methods, held in Corfu, Greece, 17-18 June 2007. All the papers have undergone further review and revision after the symposium, which has covered a number of relevant topics in the field. These include Unsteady RANS a...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor Corporativo: SpringerLink (Online service)
Otros Autores: Peng, Shia-Hui (Editor ), Haase, Werner (Editor )
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Berlin, Heidelberg : Springer Berlin Heidelberg : Imprint: Springer, 2008.
Edición:1st ed. 2008.
Colección:Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
Temas:
Acceso en línea:Texto Completo

MARC

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245 1 0 |a Advances in Hybrid RANS-LES Modelling  |h [electronic resource] :  |b Papers contributed to the 2007 Symposium of Hybrid RANS-LES Methods, Corfu, Greece, 17-18 June 2007 /  |c edited by Shia-Hui Peng, Werner Haase. 
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505 0 |a The 2007 Hybrid RANS-LES Symposium: An Outsider's View -- The 2007 Hybrid RANS-LES Symposium: An Outsider's View -- Invited Keynote Papers -- Reliability of LES in Complex Applications -- Turbulent Eddies in the RANS/LES Transition Region -- Uncertainty Modeling, Error Charts and Improvement of Subgrid Models -- Hybrid RANS-LES Modelling and Related Numerical Issues -- Hybrid LES-RANS Method Based on an Explicit Algebraic Reynolds Stress Model -- Hybrid LES-RANS: Inlet Boundary Conditions for Flows with Recirculation -- On the Use of Stimulated Detached Eddy Simulation (SDES) for Spatially Developing Boundary Layers -- Synthetic Inflow Boundary Conditions for Wall Bounded Flows -- X-LES Simulations Using a High-Order Finite-Volume Scheme -- One-Equation RG Hybrid RANS/LES Modelling -- Scrutinizing Velocity and Pressure Coupling Conditions for LES with Downstream RANS Calculations -- Comparison of Different Modelling Approaches -- Computation of the Helicopter Fuselage Wake with the SST, SAS, DES and XLES Models -- Numerical Simulation of the Flow in the Wake of Ahmed Body Using Detached Eddy Simulation and URANS Modeling -- DES and Hybrid RANS-LES Modelling of Unsteady Pressure Oscillations and Flow Features in a Rectangular Cavity -- Comparative Assessment of Hybrid LES/RANS Models in Turbulent Flows Separating from Smooth Surfaces -- Numerical Investigation of a Laboratory Combustor Applying Hybrid RANS-LES Methods -- Applications of DES and DES Variants -- DES of a Cavity with Spoiler -- DES Analysis of Confined Turbulent Swirling Flows in the Sub-critical Regime -- Zonal-Detached Eddy Simulation of Transonic Buffet on a Civil Aircraft Type Configuration -- Detached Eddy Simulation of Separated Flow on a High-Lift Device and Noise Propagation -- Unsteady CFD Analysis of a Delta Wing Fighter Configuration by Delayed Detached Eddy Simulation -- Comparison of DES and LES on the Transitional Flow of Turbine Blades -- Demonstration of Improved DES Methods for Generic and Industrial Applications -- Towards a Successful Implementation of DES Strategies in Industrial RANS Solvers -- Delayed Detached-Eddy Simulation of Supersonic Inlet Buzz -- DES Applied to an Isolated Synthetic Jet Flow -- Advanced URANS Modelling and Applications -- Development and Application of SST-SAS Turbulence Model in the DESIDER Project -- Numerical Simulation of the Dynamic Stall of a NACA 0012 Airfoil Using DES and Advanced OES/URANS Modelling -- Turbulence Modelling of Strongly Detached Unsteady Flows: The Circular Cylinder -- SGS Modelling and LES Applications -- A New Variant of Subgrid Dissipation for LES Method and Simulation of Laminar-Turbulent Transition in Subsonic Gas Flows -- Formulation of Subgrid Stochastic Acceleration Model (SSAM) for LES of a High Reynolds Number Flow -- Flow Around a Surface-Mounted Finite Cylinder: A Challenging Case for LES -- Compressibility Effects on Turbulent Separated Flow in a Streamwise-Periodic Hill Channel -- Part 2. 
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