Bandyopadhyay, K (1991) Development of transducers for aerospace structure testing using piezoelectric ceramic/polymer. Part 1 : Fabrication of accelerometer using piezoelectric ceramic. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
This report deals with the work done on the feasibility study of using piezoelectric ceramic for development of transducers for aerospace applications .For the use types of piezoelectric in aerospace structure seismic accelerometer testing two i .e ., compression and fabricated. type and bender type, The accelerometers have been utilise designed piezoelectric ceramic PZT/PLZT as transdueing material
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Piezoelectric ceramic;Accelerometer |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Materials Science Division |
| Depositing User: | Mr. N A |
| Date Deposited: | 28 Jun 2006 |
| Last Modified: | 24 May 2010 09:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1744 |
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