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FLOMANIA - A European Initiative on Flow Physics Modelling: Results of the European-Union funded project, 2002 - 2004 2006 ed. [Kõva köide]

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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 offers of the EU-funded 5th Framework project, FLOMANIA (Flow Physics Modelling - An Integrated Approach). The book presents an introduction to the project, exhibits partners' methods and approaches, and provides comprehensive reports of all applications treated in the project. A complete chapter is devoted to a description of turbulence models used by the partners together with a section on lessons learned, accompanied by a comprehensive list of references.
I The FLOMANIA Project 1(20)
1 Summary
1(1)
2 Introduction
2(3)
2.1 The basis for the FLOMANIA project
2(1)
2.2 State of the art
3(2)
3 Technical project description
5(14)
3.1 Research approach and methodology
5(2)
3.2 Dissemination and exploitation
7(1)
3.3 Description of tasks
8(9)
3.3.1 Task 1.1: Project management
8(1)
3.3.2 Task 1.2: Web server
8(1)
3.3.3 Task 2: Test case data base
9(2)
3.3.4 Task 3: Software and technology transfer
11(1)
3.3.5 Task 4.1: Modelling of Reynolds-stress models (RSM)
11(1)
3.3.6 Task 4.2: Two-equatiuon modelling
12(1)
3.3.7 Task 4.3: Sophisticated wall 'Unctions
12(1)
3.3.8 Task 4.4: DES and zonal approach
12(1)
3.3.9 Task 5.1: Implementation of turbulence models
13(1)
3.3.10 Task 5.2: Sensors for adaptation
13(1)
3.3.11 Task 5.3: Grid adaptation and grid dependence
14(1)
3.3.12 Task 5.4: Numerics and best-practice recommendations
14(1)
3.3.13 Task 6.1: Applications - generic cases – provision of meshes
15(1)
3.3.14 Task 6.1.1: Provision of meshes
15(1)
3.3.15 Task 6.1.2: RANS and URANS applications
15(1)
3.3.16 Task 6.1.3: DES applications
16(1)
3.3.17 Task 6.2: Complex applications
16(1)
3.3.18 Task 6.2.1: Rans and URANS applications
16(1)
3.3.19 Task 6.2.2: DES applications
16(1)
3.4 Task-per-partner matrix
17(1)
3.5 List of partners and addresses
18(1)
4 Conclusion
19(1)
5 The FLOMANIA Web site and the access to it
20(1)
II Technical, partner-related reports – methods, models and applications performed 21(98)
1 Contribution of ANSYS: Main achievements in FLOMANIA
21(8)
2 Contribution of Alenia: Main results obtained within the project
29(6)
3 Predictive Prospects of DES in Industrial External Aerodynamic Flow Simulations (Bombardier)
35(6)
4 Contribution of Chalmers: LES and Hybrid LES-RANS
41(4)
5 Dassault Aviation's main achievements within Flomania
45(4)
6 DLR's contribution to FLOMANIA – Methods, Models, Applications
49(8)
7 Contribution by EADS-CASA
57(6)
8 Methods and approaches used by EADS-M
63(4)
9 Method Used and Highlight Results achieved with the code_Saturne Software at EDF
67(6)
10 Contribution by FOI
73(4)
11 Contribution by ICSTM: Modelling generic 2d and 3d separated flows using anisotropy-resolving turbulence closures
77(8)
12 Advances in turbulence modelling for unsteady flows - IMFT
85(4)
13 Contribution of NUMECA: Main results achieved within the FLOMANIA project
89(6)
14 Contribution by ONERA
95(6)
15 Contribution by SPTU: Support of Partners' Efforts Directed to Implementation of DES Technology
101(8)
16 Method Used and Highlight Results Achieved in FLOMANIA (TUB)
109(4)
17 Methods used and highlighted results from UMIST
113(6)
III Presentation of turbulence models used by partners (ONERA) 119(64)
1 Models-versus-test-case matrix
119(8)
2 Eddy-viscosity turbulence models
127(15)
3 Non Linear Eddy Viscosity Models and Explicit Algebraic Reynolds Stress Models
142(12)
4 Differential reynolds stress models
154(9)
5 Wall functions
163(6)
6 Coupled RANS/LES methods
169(14)
IV Applications – test cases 183(222)
1 NACA0012 wing with rounded tip (TU Berlin)
183(10)
2 Rotor 37 (NUMECA)
193(10)
3 The Asymmetric Plane Diffuser (ICSTM)
203(16)
4 ONERA M6 wing (DLR-B)
219(6)
5 OAT15A airfoil in wind tunnel (Alenia, Dassault
225(10)
6 NACA0012 beyond stall (DLR-G)
235(12)
7 MRTT (EADS-CASA)
247(8)
8 Prediction of Cross-Wind Stability for a Generic Train (Bombardier)
255(10)
9 Analysis of Sound Sources for a Generic Car Mirror (Bombardier
265(12)
10 The TUM Forward Swept Wing Generic Aircraft (EADS-M)
277(10)
11 TUM Delta wing (Dassault)
287(12)
12 3D circular cylinder (IMFT)
299(14)
13 AS28 wing-body configuration (w/o nacelles) (ONERA)
313(12)
14 Generic air-intake (ONERA)
325(30)
15 Ahmed Car (ANSYS)
355
16 3D low hill with complex separation (Chalmers)
347(12)
17 Separation behind 2D hills (UMIST)
359(8)
18 The Aerospatiale A-airfoil (EADS-M)
367(12)
19 NACA0012 – DNS Approach (IMFT)
379(12)
20 DLR-F6 (DLR-G)
391(14)
V Summary of experience 405(16)
VI References 421


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.