TY - GEN
T1 - A Novel MEMS Sensor with a Floating Cover Plate for Wall-Shear Stress Measurement in the Harsh Supersonic Flow
AU - Liu, Yunzhe
AU - Shi, Lei
AU - Chen, Yunjian
AU - Ma, Shengming
AU - Cheng, Kai
AU - Wang, Chuqiao
AU - Zhang, Xingxu
AU - Luo, Jian
AU - Ma, Binghe
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - This work presents a novel capacitance MEMS sensor with a floating cover plate for robust wall-shear stress measurements in the harsh environment of supersonic flow field. Based on a Dual Silicon-On-Insulator (DSOI) wafer, the specific microfabrication technology is developed to achieve the combination of the floating cover plate and sensing structure, which features the accurate etching, anodic bonding, and backside TGVs' lead wire. A two-dimensional Poiseuille channel was established to carry out the sensor calibration. Moreover, the enormous reduction of damaging possibilities of the sensor in practical applications is experimentally verified. Wall-shear stress measuring experiments were performed at a Mach 2.0 supersonic wind-tunnel facility. The entire period of the supersonic flow from beginning and stabilization to end was observed by the proposed sensor, where shear stress fluctuations caused by the near-wall flow field structure were acquired. Additionally, the experimental results matched the pattern of changes in the wall pressure, and indicated the agreement with the model predictions for fully developed boundary layers.
AB - This work presents a novel capacitance MEMS sensor with a floating cover plate for robust wall-shear stress measurements in the harsh environment of supersonic flow field. Based on a Dual Silicon-On-Insulator (DSOI) wafer, the specific microfabrication technology is developed to achieve the combination of the floating cover plate and sensing structure, which features the accurate etching, anodic bonding, and backside TGVs' lead wire. A two-dimensional Poiseuille channel was established to carry out the sensor calibration. Moreover, the enormous reduction of damaging possibilities of the sensor in practical applications is experimentally verified. Wall-shear stress measuring experiments were performed at a Mach 2.0 supersonic wind-tunnel facility. The entire period of the supersonic flow from beginning and stabilization to end was observed by the proposed sensor, where shear stress fluctuations caused by the near-wall flow field structure were acquired. Additionally, the experimental results matched the pattern of changes in the wall pressure, and indicated the agreement with the model predictions for fully developed boundary layers.
KW - capacitance
KW - DSOI microfabrication
KW - floating cover plate
KW - MEMS sensor
KW - supersonic flow
KW - wall-shear stress
UR - http://www.scopus.com/inward/record.url?scp=85215275966&partnerID=8YFLogxK
U2 - 10.1109/SENSORS60989.2024.10784469
DO - 10.1109/SENSORS60989.2024.10784469
M3 - 会议稿件
AN - SCOPUS:85215275966
T3 - Proceedings of IEEE Sensors
BT - 2024 IEEE Sensors, SENSORS 2024 - Conference Proceedings
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2024 IEEE Sensors, SENSORS 2024
Y2 - 20 October 2024 through 23 October 2024
ER -