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Produktbild: Advances in Effective Flow Separation Control for Aircraft Drag Reduction
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Advances in Effective Flow Separation Control for Aircraft Drag Reduction Modeling, Simulations and Experimentations

Aus der Reihe Computational Methods in Applied Sciences

145,99 €

inkl. gesetzl. MwSt., Versandkostenfrei

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

15.11.2019

Abbildungen

X, 341 p. 285 illus., 218 illus. in color.

Herausgeber

Ning Qin + weitere

Verlag

Springer

Seitenzahl

341

Maße (L/B/H)

24,1/16/2,5 cm

Gewicht

694 g

Auflage

19001 Auflage 1st edition 2020

Sprache

Englisch

ISBN

978-3-030-29687-2

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

15.11.2019

Abbildungen

X, 341 p. 285 illus., 218 illus. in color.

Herausgeber

Verlag

Springer

Seitenzahl

341

Maße (L/B/H)

24,1/16/2,5 cm

Gewicht

694 g

Auflage

19001 Auflage 1st edition 2020

Sprache

Englisch

ISBN

978-3-030-29687-2

Herstelleradresse

Springer-Verlag GmbH
Tiergartenstr. 17
69121 Heidelberg
DE

Email: ProductSafety@springernature.com

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  • Produktbild: Advances in Effective Flow Separation Control for Aircraft Drag Reduction

  • 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



    5.6.1  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 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)




    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