Development of transducers for aerospace structure testing using piezoelectric ceramic/polymer. Part 1 : Fabrication of accelerometer using piezoelectric ceramic

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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