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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 differential Reynolds Stress models for aeronautical applications and modelling of detached-eddy simulations (DES). The book presents an introduction to the project, exhibits partners’ methods and approaches, and provides comprehensive reports (i.e. definition as well as results) of all applications treated in the project. Moreover, a complete chapter is devoted to a description of turbulence models used by the partners together with a section on lessons learnt – accompanied by a comprehensive list of references.




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 differential Reynolds Stress models for aeronautical applications and modelling of detached-eddy simulations (DES). The book presents an introduction to the project, exhibits partners’ methods and approaches, and provides comprehensive reports (i.e. definition as well as results) of all applications treated in the project. Moreover, a complete chapter is devoted to a description of turbulence models used by the partners together with a section on lessons learnt – accompanied by a comprehensive list of references.




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 differential Reynolds Stress models for aeronautical applications and modelling of detached-eddy simulations (DES). The book presents an introduction to the project, exhibits partners’ methods and approaches, and provides comprehensive reports (i.e. definition as well as results) of all applications treated in the project. Moreover, a complete chapter is devoted to a description of turbulence models used by the partners together with a section on lessons learnt – accompanied by a comprehensive list of references.


Content:
Front Matter....Pages I-XI
The FLOMANIA project....Pages 1-20
Contribution of ANSYS: Main achievements in FLOMANIA....Pages 21-28
Contribution of Alenia: Main results obtained within the project....Pages 29-34
Predictive Prospects of DES in Industrial External Aerodynamic Flow Simulations....Pages 35-40
Contribution of Chalmers: LES and Hybrid LES-RANS....Pages 41-44
Dassault Aviation’s main achievements within Flomania....Pages 45-48
DLR’s Contribution to FLOMANIA — Methods, Models, Applications....Pages 49-56
Contribution by EADS-CASA....Pages 57-62
Methods and approaches used by EADS-M....Pages 63-66
Method Used and Highlight Results achieved with the code_Saturne Software at EDF....Pages 67-72
Contribution by FOI....Pages 73-76
Contribution by ICSTM: Modelling generic 2d and 3d separated flows using anisotropy-resolving turbulence closures....Pages 77-84
Advances in turbulence modelling for unsteady flows — IMFT....Pages 85-88
Contribution of NUMECA: Main results achieved within the FLOMANIA project....Pages 89-94
Contribution by ONERA....Pages 95-100
Contribution by SPTU: Support of Partners’ Efforts Directed to Implementation of DES Technology....Pages 101-108
Method Used and Highlight Results Achieved in FLOMANIA....Pages 109-112
Methods used and highlighted results from UMIST....Pages 113-118
Models versus partners and model quick reference....Pages 119-126
Eddy-viscosity turbulence models....Pages 127-141
Non Linear Eddy Viscosity Models and Explicit Algebraic Reynolds Stress Models....Pages 142-153
Differential Reynolds stress turbulence models....Pages 154-162
Wall functions....Pages 163-168
Coupled RANS/LES methods....Pages 169-182
NACA0012 wing with rounded tip....Pages 183-192
Rotor 37....Pages 193-202
The Asymmetric Plane Diffuser....Pages 203-218
ONERA M6 wing....Pages 219-224
OAT15A airfoil in wind tunnel (Alenia, Dassault)....Pages 225-232
NACA0012 beyond Stall....Pages 233-246
MRTT....Pages 247-254
Prediction of Cross-Wind Stability for a Generic Train....Pages 255-264
Analysis of Sound Sources for a Generic Car Mirror....Pages 265-276
The TUM Forward-Swept Wing Generic Aircraft....Pages 277-286
TUM Delta wing....Pages 287-298
3D circular cylinder....Pages 299-312
AS28 wing-body configuration (w/o nacelles)....Pages 313-324
Generic air intake (ONERA)....Pages 325-334
Ahmed Car....Pages 335-346
3D low hill with complex separation....Pages 347-358
Separation behind 2d hills....Pages 359-366
The Aerospatiale A-airfoil....Pages 367-378
NACA0012 — DNS Approach....Pages 379-390
DLR F6....Pages 391-404
Summary of experience....Pages 405-420
References....Pages 421-433
Back Matter....Pages 434-435


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 differential Reynolds Stress models for aeronautical applications and modelling of detached-eddy simulations (DES). The book presents an introduction to the project, exhibits partners’ methods and approaches, and provides comprehensive reports (i.e. definition as well as results) of all applications treated in the project. Moreover, a complete chapter is devoted to a description of turbulence models used by the partners together with a section on lessons learnt – accompanied by a comprehensive list of references.


Content:
Front Matter....Pages I-XI
The FLOMANIA project....Pages 1-20
Contribution of ANSYS: Main achievements in FLOMANIA....Pages 21-28
Contribution of Alenia: Main results obtained within the project....Pages 29-34
Predictive Prospects of DES in Industrial External Aerodynamic Flow Simulations....Pages 35-40
Contribution of Chalmers: LES and Hybrid LES-RANS....Pages 41-44
Dassault Aviation’s main achievements within Flomania....Pages 45-48
DLR’s Contribution to FLOMANIA — Methods, Models, Applications....Pages 49-56
Contribution by EADS-CASA....Pages 57-62
Methods and approaches used by EADS-M....Pages 63-66
Method Used and Highlight Results achieved with the code_Saturne Software at EDF....Pages 67-72
Contribution by FOI....Pages 73-76
Contribution by ICSTM: Modelling generic 2d and 3d separated flows using anisotropy-resolving turbulence closures....Pages 77-84
Advances in turbulence modelling for unsteady flows — IMFT....Pages 85-88
Contribution of NUMECA: Main results achieved within the FLOMANIA project....Pages 89-94
Contribution by ONERA....Pages 95-100
Contribution by SPTU: Support of Partners’ Efforts Directed to Implementation of DES Technology....Pages 101-108
Method Used and Highlight Results Achieved in FLOMANIA....Pages 109-112
Methods used and highlighted results from UMIST....Pages 113-118
Models versus partners and model quick reference....Pages 119-126
Eddy-viscosity turbulence models....Pages 127-141
Non Linear Eddy Viscosity Models and Explicit Algebraic Reynolds Stress Models....Pages 142-153
Differential Reynolds stress turbulence models....Pages 154-162
Wall functions....Pages 163-168
Coupled RANS/LES methods....Pages 169-182
NACA0012 wing with rounded tip....Pages 183-192
Rotor 37....Pages 193-202
The Asymmetric Plane Diffuser....Pages 203-218
ONERA M6 wing....Pages 219-224
OAT15A airfoil in wind tunnel (Alenia, Dassault)....Pages 225-232
NACA0012 beyond Stall....Pages 233-246
MRTT....Pages 247-254
Prediction of Cross-Wind Stability for a Generic Train....Pages 255-264
Analysis of Sound Sources for a Generic Car Mirror....Pages 265-276
The TUM Forward-Swept Wing Generic Aircraft....Pages 277-286
TUM Delta wing....Pages 287-298
3D circular cylinder....Pages 299-312
AS28 wing-body configuration (w/o nacelles)....Pages 313-324
Generic air intake (ONERA)....Pages 325-334
Ahmed Car....Pages 335-346
3D low hill with complex separation....Pages 347-358
Separation behind 2d hills....Pages 359-366
The Aerospatiale A-airfoil....Pages 367-378
NACA0012 — DNS Approach....Pages 379-390
DLR F6....Pages 391-404
Summary of experience....Pages 405-420
References....Pages 421-433
Back Matter....Pages 434-435
....
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