AeroMEMS sensor array for high-resolution wall pressure measurements

被引:62
作者
Berns, A.
Buder, U.
Obermeier, E.
Wolter, A.
Leder, A.
机构
[1] Tech Univ Berlin, MAT, D-13355 Berlin, Germany
[2] Univ Rostock, Dept Fluid Mech, D-2500 Rostock, Germany
关键词
AeroMEMS; pressure sensor; wall pressure; fluid mechanics;
D O I
10.1016/j.sna.2006.04.056
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
The measurement of wall pressure and wall pressure fluctuations in fluid mechanics is of great importance for the investigation of turbulent flow phenomena. This paper is focused on the design, fabrication and test of a micro electromechanical system (MEMS) pressure sensor array for high-resolution wall pressure measurements in turbulent flows. In contrast to pressure sensor arrays in literature this array is highly sensitive and can be flush mounted on top of a cylinder without using pin holes and flexible tubes. Employing silicon-on-insulator (SOI) technology and deep silicon etching the sensors developed achieve a pressure resolution of 0.5 Pa. Three different types of sensors, featuring a diaphragm thickness of 3 mu m and diaphragm sizes of 500 mu m, 700 mu m, and 900 mu m (square diaphragm), have been fabricated and characterized. Simulation of the dynamic behavior yields resonance frequencies of 50 kHz (900 mu m-diaphragm), 82 kHz (700 mu m-diaphragm), and 160 kHz (500 mu m-diaphragm). Sensitivities of 12 mu V/(VPa) (900 mu m-sensor), 7 mu V/(VPa) (700 mu m-sensor), and 3 mu V/(VPa) (500 mu m-sensor) are obtained in measurement ranges of +/- 200 Pa, +/- 500 Pa, and +/- 1 kPa, respectively, featuring a non-linearity of less than 1%. The array was flush mounted on a cylinder (radius 60 mm, height 240 mm) and tested in a wind tunnel. (c) 2006 Elsevier B.V. All rights reserved.
引用
收藏
页码:104 / 111
页数:8
相关论文
共 19 条
[1]  
ARNOLD DP, 2001, P ASME INT MECH ENG, P281
[2]  
BOONE AR, 2002, 22 AIAA AER MEAS TEC
[3]   AN ULTRASENSITIVE SILICON PRESSURE-BASED MICROFLOW SENSOR [J].
CHO, ST ;
NAJAFI, K ;
LOWMAN, CE ;
WISE, KD .
IEEE TRANSACTIONS ON ELECTRON DEVICES, 1992, 39 (04) :825-835
[4]   A MODEL FOR BORON SHORT-TIME ANNEALING AFTER ION-IMPLANTATION [J].
HANE, M ;
MATSUMOTO, H .
IEEE TRANSACTIONS ON ELECTRON DEVICES, 1993, 40 (07) :1215-1222
[5]  
Johansen ES, 2003, 41 AER SCI M EXH REN
[6]   VERIFICATION OF ANALYTIC POINT-DEFECT MODELS USING SUPREM-IV [J].
LAW, ME ;
DUTTON, RW .
IEEE TRANSACTIONS ON COMPUTER-AIDED DESIGN OF INTEGRATED CIRCUITS AND SYSTEMS, 1988, 7 (02) :181-190
[7]   Flex circuit sensor array for surface unsteady pressure measurements [J].
Leger, TJ ;
Johnston, DA ;
Wolff, JM .
JOURNAL OF PROPULSION AND POWER, 2004, 20 (04) :754-758
[8]  
LIWEI L, 1998, P IEEE AER C SNOWM A, P429
[9]   MEMS applications in turbulence and flow control [J].
Löfdahl, L ;
Gad-el-Hak, M .
PROGRESS IN AEROSPACE SCIENCES, 1999, 35 (02) :101-203
[10]   A silicon piezoresistive pressure sensor [J].
Singh, R ;
Ngo, LL ;
Seng, HS ;
Mok, FNC .
FIRST IEEE INTERNATION WORKSHOP ON ELECTRONIC DESIGN, TEST AND APPLICATIONS, PROCEEDINGS, 2002, :181-184