DocumentCode
1026762
Title
Microsensors and actuators for macrofluidic control
Author
Huang, Adam ; Lew, James ; Xu, Yong ; Tai, Yu-Chong ; Ho, Chih-Ming
Author_Institution
Mech. & Aerosp. Dept., Univ. of California, Los Angeles, CA, USA
Volume
4
Issue
4
fYear
2004
Firstpage
494
Lastpage
502
Abstract
Microsensors and actuators suitable for macrofluidic control have been designed, fabricated, tested, and optimized over the span of the last decade. MEMS-based shear stress sensor arrays using polysilicon hot filaments have been fabricated on both rigid (silicon) and flexible (parylene) substrate for application on all types of fluid dynamic and aerodynamic surfaces. In addition, MEMS bubble flap-type pneumatic actuators have been tested and used in turbulent boundary layer drag reduction in conjunction with the rigid MEMS shear stress sensor arrays acting as high-speed shear stress imagers. The flexible MEMS bubble actuator arrays have also been used with the flexible shear stress sensor arrays for generating maneuvering forces in the wind tunnel for a delta wing model and on UAV-type radio-controlled aircraft.
Keywords
boundary layer turbulence; drag reduction; microactuators; microfluidics; microsensors; pneumatic actuators; MEMS-based shear stress sensor arrays; UAV-type radio-controlled aircraft; aerodynamic surfaces; bubble actuator arrays; bubble flap-type pneumatic actuators; delta wing model; flexible parylene substrate; fluid dynamic surfaces; macrofluidic control; maneuvering force generation; microsensors; polysilicon hot filaments; rigid silicon substrate; shear stress imagers; turbulent boundary layer drag reduction; vortex shifting concept; wind tunnel; Actuators; Aerodynamics; Design optimization; Fluid dynamics; Micromechanical devices; Microsensors; Sensor arrays; Silicon; Stress; Testing; Macrofluidic control; TBL; VSC; drag reduction; turbulent boundary layer; vortex shifting concept;
fLanguage
English
Journal_Title
Sensors Journal, IEEE
Publisher
ieee
ISSN
1530-437X
Type
jour
DOI
10.1109/JSEN.2004.830949
Filename
1310342
Link To Document