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