Del 52 i serien Computational Methods in Applied Sciences

Advances in Effective Flow Separation Control for Aircraft Drag Reduction

Modeling, Simulations and Experimentations

Häftad, Engelska, 2020

AvNing Qin,Jacques Periaux,Gabriel Bugeda

2 109 kr

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This book presents the results of a European-Chinese collaborative research project, Manipulation of Reynolds Stress for Separation Control and Drag Reduction (MARS), including an analysis and discussion of the effects of a number of active flow control devices on the discrete dynamic components of the turbulent shear layers and Reynolds stress.

Produktinformation

Utgivningsdatum2020-11-15
Mått155 x 235 x 24 mm
Vikt536 g
FormatHäftad
SpråkEngelska
SerieComputational Methods in Applied Sciences
Antal sidor341
FörlagSpringer Nature Switzerland AG
ISBN9783030296902

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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 experimentation6.4.1 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 experimentation6.5.1 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 optimization5.6.1 Plasma ( Ning Qin, Univ. Sheffield, UK ) (2) 5.6.2 Synthetic Jets (NUAA , China) (2)5.7 NACA0015: definition of active device test case optimization5.7.1 Pulsed Jets ( Univ. Poitiers ) (2)5.8: Experimentations and simulations of BSF test cases: contributions5.8.1 Contributed experimentations (7x 12= 84)5.8.2 Contributed simulations (9)5.9 : experimentations and simulations of NACA0015 test cases : contributions 5.9.1: Contributed experimentations (5x12= 60) 5.9.2 Contributed simulations ( 10x12= 120) 5.10: Optimization of the active devices on BSF test cases: contributions (4x12=48) 5.11: Optimization of the active devices on NACA0015 test cases: contributions (5x12= 60)6. Analysis and synthesis of the achieved experimental, computational and active devices optimization contributions on BSF and NACA00126 .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)7. Assessment of results obtained in the MARS project (Herman Deconinck, VKI, Belgium, Yao Zheng , Zhejiang University , China ) ( 2x2=4)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