Microsensors and actuators for macrofluidic control

被引:24
作者
Huang, A [1 ]
Lew, J
Xu, Y
Tai, YC
Ho, CM
机构
[1] Univ Calif Los Angeles, Mech & Aerosp Dept, Los Angeles, CA 90095 USA
[2] Wayne State Univ, Dept Elect & Comp Engn, Detroit, MI 48202 USA
[3] CALTECH, Pasadena, CA 91125 USA
基金
美国国家航空航天局;
关键词
macrofluidic control; turbulent boundary layer (TBL) drag reduction; vortex shifting concept (VSC);
D O I
10.1109/JSEN.2004.830949
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
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 highspeed 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.
引用
收藏
页码:494 / 502
页数:9
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