Manufacturing Technology Today

Open Access Open Access  Restricted Access Subscription Access
Open Access Open Access Open Access  Restricted Access Restricted Access Subscription Access

Measurement of Static Pressure Over Bodies in Hypersonic Shock Tunnel Using MEMS-based Pressure Sensor Array


Affiliations
1 Dept. of Aerospace Engg, Indian Institute of Science, Bangalore, India
2 Indian Space Research Organisation, Dept. of Space, Bangalore, India
     

   Subscribe/Renew Journal


This paper reports on development of MEMS based pressure sensors arrays for static pressure measurement on aerodynamic surfaces. The two different types of sensors arrays with cluster of 25 sensors and 5 sensors are developed. The characterization of pressure sensors arrays carried out in static condition and the working of sensors has been demonstrated for hypersonic flows in shock tunnel with the cluster of 5 sensors array. The static pressure measured using the MEMS sensors in shock tunnel testing are in good agreement with conventional Kulite sensors.

Keywords

Pressure Measurements, MEMS Sensors, Hypersonic Flow, Pressure Sensor.
User
Subscription Login to verify subscription
Notifications
Font Size

Abstract Views: 198

PDF Views: 0




  • Measurement of Static Pressure Over Bodies in Hypersonic Shock Tunnel Using MEMS-based Pressure Sensor Array

Abstract Views: 198  |  PDF Views: 0

Authors

S. N. Ram
Dept. of Aerospace Engg, Indian Institute of Science, Bangalore, India
Jaspreet Singh
Dept. of Aerospace Engg, Indian Institute of Science, Bangalore, India
G. Jagadeesh
Dept. of Aerospace Engg, Indian Institute of Science, Bangalore, India
M. M. Nayak
Indian Space Research Organisation, Dept. of Space, Bangalore, India
K. Nagachenchaiah
Indian Space Research Organisation, Dept. of Space, Bangalore, India

Abstract


This paper reports on development of MEMS based pressure sensors arrays for static pressure measurement on aerodynamic surfaces. The two different types of sensors arrays with cluster of 25 sensors and 5 sensors are developed. The characterization of pressure sensors arrays carried out in static condition and the working of sensors has been demonstrated for hypersonic flows in shock tunnel with the cluster of 5 sensors array. The static pressure measured using the MEMS sensors in shock tunnel testing are in good agreement with conventional Kulite sensors.

Keywords


Pressure Measurements, MEMS Sensors, Hypersonic Flow, Pressure Sensor.