Recent progress in flow control for practical flows : results of the STADYWICO and IMESCON Projects

This book explores the outcomes on flow control research activities carried out within the framework of two EU-funded projects focused on training-through-research of Marie Sklodowska-Curie doctoral students. The main goal of the projects described in this monograph is to assess the potential of the...

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Bibliographic Details
Other Authors Doerffer, Piotr (Editor), Barakos, George N. (Editor), Luczak, Marcin M. (Editor)
Format Electronic eBook
LanguageEnglish
Published Cham, Switzerland : Springer, 2017.
Subjects
Fluid power technology.
Automatic control.
elektronické knihy
electronic books
Online AccessFull text
ISBN9783319505688
9783319505671
Physical Description1 online resource (xi, 511 pages) : illustrations (some color)

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245 0 0 |a Recent progress in flow control for practical flows :  |b results of the STADYWICO and IMESCON Projects /  |c Piotr Doerffer, George N. Barakos, Marcin M. Luczak, editors. 
264 1 |a Cham, Switzerland :  |b Springer,  |c 2017. 
300 |a 1 online resource (xi, 511 pages) :  |b illustrations (some color) 
336 |a text  |b txt  |2 rdacontent 
337 |a počítač  |b c  |2 rdamedia 
338 |a online zdroj  |b cr  |2 rdacarrier 
505 0 |a Acknowledgements; Contents; Part I Introduction to Flow Control Technology; 1 Introduction and Literature Survey; 1.1 Introduction; 1.2 Vortex Generators; 1.3 Air-Jet Vortex Generators; 1.4 Synthetic Jets; 1.5 Surface Blowing Circulation; 1.6 Surface Suction; 1.7 Plasma Technology; 1.8 Nonfluidic Devices; 1.8.1 Leading Edge Geometries; 1.8.2 Trailing Edge Flaps: Gurney Flaps; 1.8.2.1 Actuation Mechanism; 1.9 Conclusions; References; Part II Design of Modern Gurney Flap; 2 CFD Method for Modelling Gurney Flaps; 2.1 Numerical Methods; 2.1.1 HMB Solver; 2.1.2 Modelling Gurney Flaps. 
505 8 |a 2.1.2.1 Proposed Methods2.1.2.2 Implementation of the Gurney flaps; 2.1.3 Results for Gurney Flaps in Two Dimensions; 2.1.3.1 Fixed Gurney Flap; 2.1.3.2 Resolving Flow Details Near the Gurney Flap; 2.1.3.3 Comparison Against Thick Gurney Flap; 2.2 3D Computations: Gurney Flaps vs Vortex Generators, Comparison Study of Aerodynamic Characteristics; 2.2.1 Static Computations; 2.2.2 Pitching-Translating Wing Computations; 2.2.3 Observations; References; 3 Performance Enhancement of Rotors in Hover Using Fixed Gurney Flaps; Nomenclature; Latin; Greek; Acronyms; 3.1 Numerical Methods. 
505 8 |a 3.1.1 Modelling Gurney Flaps3.1.2 Coupling with Structural Dynamics; 3.1.3 Trimming Method; 3.2 Hover Flight Calculations; 3.2.1 W3-Sokol MRB Geometry; 3.2.2 Rigid Blade Computations; 3.2.2.1 Performance; 3.2.2.2 Analysis of Rigid Blade Results; 3.2.3 Aeroelastic Calculations; 3.2.3.1 Application of the Aeroelastic Method and Trimming; 3.2.3.2 Analysis of Elastic Blade Results; 3.3 Conclusions; References; 4 Alleviation of Retreating Side Stall Using Active Gurney Flaps; Nomenclature; Latin; Greek; Acronyms; 4.1 Introduction; 4.2 Numerical Methods; 4.2.1 Coupling with Structural Dynamics. 
505 8 |a 4.2.2 Trimming Method4.3 W3 Main Rotor; 4.4 Flight Test Data; 4.5 Forward Flight; 4.5.1 Rigid Blade; 4.5.2 Elastic Blade; 4.6 Conclusions; References; 5 Effect of Gurney Flaps on Overall Helicopter Flight Envelope; Nomenclature; Latin; Greek; Acronyms; 5.1 Gurney Effect on Structural Properties of the Blade; 5.2 Closed Loop Control; 5.2.1 2D Closed Loop Control; 5.2.2 W3-Sokol Closed Loop Control; 5.3 Effect of Gurney Flap on Full Helicopter Model; 5.3.1 FLIGHTLAB Model; 5.3.2 FLIGHTLAB Validation; 5.3.3 Designed Controller for Closed Loop Analysis. 
505 8 |a 5.3.4 Synthesis of Control Law with Observers5.3.5 Handling Qualities; 5.4 Conclusions and Future Work; References; 6 Active Gurney Flap Unit; 6.1 Introduction; 6.2 Gurney Flap Actuation Mechanism Concept; 6.2.1 Position Analysis; 6.2.2 Velocity Analysis; 6.2.3 Dynamic Force Analysis; 6.3 Blade Section with Active Gurney Flap; 6.4 Conclusions; References; 7 Gurney Flap Force Calculations; 7.1 Introduction; 7.2 Retracting Gurney Flap; 7.3 Solution Methodology; 7.4 Results; 7.5 Conclusion; References; Part III Design of Rod Vortex Generator. 
500 |a Includes index. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |a This book explores the outcomes on flow control research activities carried out within the framework of two EU-funded projects focused on training-through-research of Marie Sklodowska-Curie doctoral students. The main goal of the projects described in this monograph is to assess the potential of the passive- and active-flow control methods for reduction of fuel consumption by a helicopter. The research scope encompasses the fields of structural dynamics, fluid flow dynamics, and actuators with control. Research featured in this volume demonstrates an experimental and numerical approach with a strong emphasis on the verification and validation of numerical models. The book is ideal for engineers, students, and researchers interested in the multidisciplinary field of flow control. Provides highly relevant and up-to-date information on the topic of flow control; Includes assessments of a wide range of flow-control technologies and application examples for fixed and rotary-wing configurations; Reinforces reader understanding with case studies based on real aircraft; Explains modelling methodologies and strategies for flow control of separated flows and numerous experimental measurement results on the real structures; Illustrates new developments in actuator technology. 
590 |a SpringerLink  |b Springer Complete eBooks 
650 0 |a Fluid power technology. 
650 0 |a Automatic control. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Doerffer, Piotr,  |e editor. 
700 1 |a Barakos, George N.,  |e editor. 
700 1 |a Luczak, Marcin M.,  |e editor. 
776 0 8 |i Print version:  |t Recent progress in flow control for practical flows.  |d Cham, Switzerland : Springer, 2017  |z 331950567X  |z 9783319505671  |w (OCoLC)962351217 
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999 |c 100082  |d 100082 
993 |x NEPOSILAT  |y EIZ 

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