FLOMANIA — A European Initiative on Flow Physics Modelling Results of the European-Union funded project, 2002 – 2004 /
This volume contains results gained from the EU-funded 5th Framework project, FLOMANIA (Flow Physics Modelling – An Integrated Approach). 17 European organisations, industry, research, and universities, have collaborated on topics of improvement of existing methods, investigation and integration of...
Συγγραφή απο Οργανισμό/Αρχή: | |
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Άλλοι συγγραφείς: | , , , |
Μορφή: | Ηλεκτρονική πηγή Ηλ. βιβλίο |
Γλώσσα: | English |
Έκδοση: |
Berlin, Heidelberg :
Springer Berlin Heidelberg,
2006.
|
Σειρά: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM),
94 |
Θέματα: | |
Διαθέσιμο Online: | Full Text via HEAL-Link |
Πίνακας περιεχομένων:
- 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.