Advances in Effective Flow Separation Control for Aircraft Drag Reduction
Springer International Publishing (Verlag)
978-3-030-29690-2 (ISBN)
1. Preface ( 2)
2. Foreword 1 (Norman Wood, Airbus) (2)
3. Foreword 2 (Dietrich Knoerzer ,EC Brussels and LI Benjian, MIIT Beijing ) (2)
4. Introduction.4.1 Flow Control Active devices : experimental state of the art ( J.P. Bonnet, Poitiers , France) (15)
4.2 Flow Control Active devices: numerical state of the art (FU Song, Tsinghua University, Beijing (15)5. Overview of the MARS project : overview and outcomes ( Ning Qin , Univ. Sheffield , UK and Dong Jun, ARI, China) (15)
6. MARS Evaluation : The Database Workshop ( Jacques Periaux , Gabriel Bugeda and Jordi Pons, , CIMNE, Spain)
6.1 Motivation, objectives , experimental and computational data ( Ning Qin, University of Sheffield, Spain ) (5)
6.2 The MARS Database: structure , access and regulations (Jordi Pons, CIMNE, Spain) (5)
6.3 The MARS Database content : BSF and NACA 0015 test cases definition , experimentation simulation and optimization (5)
6.4 .BFS : definition of test cases for simulation and experimentation
6.4.1 Oscillating surfaces( UNIMAN, UK) (2)
6.4.2 Plasma ( UNIMAN , UK ,Univ Poitiers, France and DLR-Gottingen, Germany) (2)6.4.3 Synthetic jets ( x NPU, China and y NUAA) (2)
6.4.4 Micro blowing/suction ( Ming Xiao, NUAA, China) (2)
6.4.5 Spanwise vortex generators ( Ming Xiao, NUAA, China) (2)
6.5 NACA0015 : definition of test cases for simulation and experimentation
6.5.1 Plasma ( x, AVIC-ARI, China ) (2)6.5.2 Synthetic Jets ( x, AVIC-ARI, China) (2)
6.5.3 Moving surfaces (x, AVIC-ARI, China) (2)
6.5.4 Micro blowing/suction ( x BUAA , China) (2)
6.5.5 Pulsed jets (x Univ. Poitiers, France) (2)5.6 BFS: definition of active device test case optimization
6. Analysis and synthesis of the achieved experimental, computational and active devices optimization contributions on BSF and NACA0012
6 .1 Academic point of view ( Adel Abbas , UPM & Airbus, Ning Qin , Univ. Sheffield, UK and Dong Jun, ARI, China, Jean Paul Bonnet , Univ. Poitiers , FU Song , Tsinghua University, Beijing, China , Ming Xiao, NUAA, China, Gao Zhenghong , NPU, China, Peng Shi-Hua , FOA, Sweden) (8x3=24)
6.2 Industrial point of view ( Norman Wood, Airbus; Jean Claude Courty Dassault Aviation , France ; Nicola Ceresola , Alenia ,Italy; DENG Yiju, FAI, China, Meihong Zhong, COMAC, China, Charles Hirsch, NUMECA, Belgium) (6x3= 18)
8. Conclusion and future ( Ning Qin , Sheffield University, UK and Dong Jun , ARI, China) (2)
9. Acknowledgements (1)
10. References (2)
11. Index of authors
Erscheinungsdatum | 17.11.2020 |
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Reihe/Serie | Computational Methods in Applied Sciences |
Zusatzinfo | X, 341 p. 285 illus., 218 illus. in color. |
Verlagsort | Cham |
Sprache | englisch |
Maße | 155 x 235 mm |
Gewicht | 539 g |
Themenwelt | Technik ► Luft- / Raumfahrttechnik |
Schlagworte | Active flow control • Backward Facing Step and Airfoil • Hybrid RANS-LES • Mars • optimization techniques • Separation Control |
ISBN-10 | 3-030-29690-3 / 3030296903 |
ISBN-13 | 978-3-030-29690-2 / 9783030296902 |
Zustand | Neuware |
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