FLOMANIA - A European Initiative on Flow Physics Modelling

All editors have been working for several decades in the books’ field of interest and are, thus, well aware of the current state-of-the-art in CFD and turbulence modelling in particular.

• The FLOMANIA project.- The FLOMANIA project.- Technical, partner-related reports — methods, models and applications performed.- Contribution of ANSYS: Main achievements in FLOMANIA.- Contribution of Alenia: Main results obtained within the project.- Predictive Prospects of DES in Industrial External Aerodynamic Flow Simulations.- Contribution of Chalmers: LES and Hybrid LES-RANS.- Dassault Aviation’s main achievements within Flomania.- DLR’s Contribution to FLOMANIA — Methods, Models, Applications.- Contribution by EADS-CASA.- Methods and approaches used by EADS-M.- Method Used and Highlight Results achieved with the code_Saturne Software at EDF.- Contribution by FOI.- Contribution by ICSTM: Modelling generic 2d and 3d separated flows using anisotropy-resolving turbulence closures.- Advances in turbulence modelling for unsteady flows — IMFT.- Contribution of NUMECA: Main results achieved within the FLOMANIA project.- Contribution by ONERA.- Contribution by SPTU: Support of Partners’ Efforts Directed to Implementation of DES Technology.- Method Used and Highlight Results Achieved in FLOMANIA.- Methods used and highlighted results from UMIST.- Presentation of turbulence models used by partners.- Models versus partners and model quick reference.- Eddy-viscosity turbulence models.- Non Linear Eddy Viscosity Models and Explicit Algebraic Reynolds Stress Models.- Differential Reynolds stress turbulence models.- Wall functions.- Coupled RANS/LES methods.- Applications — test cases.- NACA0012 wing with rounded tip.- Rotor 37.- The Asymmetric Plane Diffuser.- ONERA M6 wing.- OAT15A airfoil in wind tunnel (Alenia, Dassault).- NACA0012 beyond Stall.- MRTT.- Prediction of Cross-Wind Stability for a Generic Train.- Analysis of Sound Sources for a Generic Car Mirror.-The TUM Forward-Swept Wing Generic Aircraft.- TUM Delta wing.- 3D circular cylinder.- AS28 wing-body configuration (w/o nacelles).- Generic air intake (ONERA).- Ahmed Car.- 3D low hill with complex separation.- Separation behind 2d hills.- The Aerospatiale A-airfoil.- NACA0012 — DNS Approach.- DLR F6.- Summary of experience.- Summary of experience.- Physical and numerical upgrades in the Detached-Eddy Simulation of complex turbulent flows.- References.