《Recent Progress in Flow Control for Practical Flows: Results of the STADYW...
《Recent Progress in Flow Control for Practical Flows: Results of the STADYWICO and IMESCON Projects》实际流量的流量控制的研究进展：STADYWICO和IMESCON项目结果
编者：
Piotr Doerffer
George N. Barakos
Marcin M. Luczak
出版社：Springer
出版时间：2017年
目录
Part I Introduction to Flow Control Technology
1 Introduction and Literature Survey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
Vasileios Pastrikakis and George Barakos
Part II Design of Modern Gurney Flap
2 CFD Method forModelling Gurney Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
Vasileios Pastrikakis, Mark Woodgate, and George Barakos
3 Performance Enhancement of Rotors in Hover Using Fixed
Gurney Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 51
Vasileios Pastrikakis, René Steijl, and George Barakos
4 Alleviation of Retreating Side Stall Using Active Gurney Flaps . . . . . . 69
Vasileios Pastrikakis, René Steijl, and George Barakos
5 Effect of Gurney Flaps on Overall Helicopter Flight Envelope . . . . . . . 87
Vasileios Pastrikakis and George Barakos
6 Active Gurney Flap Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 105
Ihor Berezin and R. Raczynski
7 Gurney Flap Force Calculations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 121
Prasanta Sarkar and Radoslaw Raczynski
Part III Design of Rod Vortex Generator
8 Investigation of Vortex Generators on Channels and Airfoils . . . . . . . . . 137
Fernando Tejero, Piotr Doerffer, Pawel Flaszynski, and Oskar Szulc
ix
x Contents
9 Implementation of Rod Vortex Generators on Helicopter
Rotor Blades in Hover and Forward Flight Conditions . . . . . . . . . . . . . . . . 155
Fernando Tejero, Piotr Doerffer, Paweł Flaszy´nski, and Oskar Szulc
10 Retractable Rod Vortex Generator .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 175
Tomasz Lewandowski
Part IV Important Issues in Synthetic Jet Design
11 Numerical Simulation of a Synthetic Jet Actuator
for Active Flow Control .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 203
Marcin Kurowski
12 Introduction to the Synthetic Jet Flow Control and Drag
Reduction Techniques . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 223
Milan Matejka
13 Experimental Results of Synthetic JetWind Tunnel Tests . . . . . . . . . . . . . 233
Milan Matejka
Part V Multi Physics Co-simulation Methods
14 Fluid –Structure Interaction Simulation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 263
Ihor Berezin, Prasanta Sarkar, and Jacek Malecki
15 Analysis and Optimization of Flow Around FlexibleWings and
Blades Using the Standard Co-simulation InterfaceMpCCI. . . . . . . . . . 283
Nadja Wirth, Pascal Bayrasy, Bettina Landvogt, Klaus Wolf,
Francesco Cecutti, and Tomasz Lewandowski
16 Numerical Simulation of Airflow and Acoustic Field Around
a Passenger Car Model Using Euler Approach and Hybrid Meshing 323
Oskar Szulc and Piotr Doerffer
17 Computation of Rotorcraft Stability Derivatives Using
the Discrete Adjoint Method . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 337
M. Biava and G. Barakos
Part VI Structural Dynamics of Blades and Components
18 Dynamics of the Synthetic Jet Actuator Investigation
by the Numerical and Experimental Approach . . . . . . . . . . . . . . . . . . . . . . . . . 359
R¯uta Rimašauskien˙e
19 Thermal Synthetic Jet Actuator Investigation by Experimental
Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 375
R¯uta Rimašauskien˙e
20 Modal Analysis of PZL-W-3/W-3A Sokol Main Rotor . . . . . . . . . . . . . . . . . 395
Ihor Berezin
Contents xi
21 Strain Modal Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 405
Fabio L.M. dos Santos and Bart Peeters
22 Uncertainty Quantification of the Main Rotor Blades
Measurements. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 429
Marcin M. Luczak
23 Temperature Compensation Methods for Elastic Wave Based SHM . 483
Codru¸t Alexandru Dan and PawełKudela
Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 499
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