Design of a high-lift experiment in water including active flow control

被引:7
作者
Beutel, T. [1 ]
Sattler, S. [2 ]
El Sayed, Y. [2 ]
Schwerter, M. [1 ]
Zander, M. [3 ]
Buetgenbach, S. [1 ]
Leester-Schaedel, M. [1 ]
Radespiel, R. [2 ]
Sinapius, M. [3 ]
Wierach, P. [4 ]
机构
[1] Tech Univ Carolo Wilhelmina Braunschweig, Inst Microtechnol IMT, D-38124 Braunschweig, Germany
[2] Tech Univ Carolo Wilhelmina Braunschweig, Inst Fluid Mech ISM, D-38108 Braunschweig, Germany
[3] Tech Univ Carolo Wilhelmina Braunschweig, Inst Adaptron & Funct Integrat IAF, D-38106 Braunschweig, Germany
[4] Deutsch Zentrum Luft & Raumfahrt eV DLR, Inst Composite Struct & Adapt Syst IFA, D-38108 Braunschweig, Germany
关键词
MEMS pressure and wall shear stress sensor; active flow control; piezoelectric actuator;
D O I
10.1088/0964-1726/23/7/077004
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
This paper describes the structural design of an active flow-control experiment. The aim of the experiment is to investigate the increase in efficiency of an internally blown Coanda flap using unsteady blowing. The system uses tailor-made microelectromechanical (MEMS) pressure sensors to determine the state of the oncoming flow and an actuated lip to regulate the mass flow and velocity of a stream near a wall over the internally blown flap. Sensors and actuators are integrated into a highly loaded system that is extremely compact. The sensors are connected to a bus system that feeds the data into a real-time control system. The piezoelectric actuators using the d(33) effect at a comparable low voltage of 120 V are integrated into a lip that controls the blowout slot height. The system is designed for closed-loop control that efficiently avoids flow separation on the Coanda flap. The setup is designed for water-tunnel experiments in order to reduce the free-stream velocity and the system's control frequency by a factor of 10 compared with that in air. This paper outlines the function and verification of the system's main components and their development.
引用
收藏
页数:10
相关论文
共 20 条
[1]  
[Anonymous], 2012, PICMA STACK MULTILAY
[2]  
Behr C, 2013, ENTWURF CHARACTERISI
[3]  
BEUTEL T, 2010, SENSORS TRANSDUCERS, V115, P11
[4]  
Burnazzi M, 2013, P 51 AIAA AER SCI M
[5]   Feedback control of a cylinder wake low-dimensional model [J].
Cohen, K ;
Siegel, S ;
McLaughlin, T ;
Gillies, E .
AIAA JOURNAL, 2003, 41 (07) :1389-1391
[6]  
Gad-el-Hak M., 2002, The MEMS Handbook, V2
[7]   Numerical Investigation of Leading Edge Blowing and Optimization of the Slot Geometry for a Circulation Control Airfoil [J].
Jensch, C. ;
Pfingsten, K. C. ;
Radespiel, R. .
NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS VII, 2010, 112 :183-190
[8]  
Jensch C, 2009, P DLRK 2009 AACH
[9]  
Jones G S, 2003, 21 AIAA APPL AER C O
[10]  
Keller D, 2013, CFF FORSCHUNGSBERICH, P147