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Passively Damped Laminated Piezoelectric Shell Structures with Integrated Electric Networks

AUTHOR Nasa, National Aeronautics and Space Adm
PUBLISHER Independently Published (09/25/2018)
PRODUCT TYPE Paperback (Paperback)

Description
Multi-field mechanics are presented for curvilinear piezoelectric laminates interfaced with distributed passive electric components. The equations of motion for laminated piezoelectric shell structures with embedded passive electric networks are directly formulated and solved using a finite element methodology. The modal damping and frequencies of the piezoelectric shell are calculated from the poles of the system. Experimental and numerical results are presented for the modal damping and frequency of composite beams with a resistively shunted piezoceramic patch. The modal damping and frequency of plates, cylindrical shells and cylindrical composite blades with piezoelectric-resistor layers are predicted. Both analytical and experimental studies illustrate a unique dependence of modal damping and frequencies on the shunting resistance and show the effect of structural shape and curvature on piezoelectric damping. Saravanos, Dimitris A. Glenn Research Center NASA/CR-1999-208871, NAS 1.26:208871, E-11515
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Product Details
ISBN-13: 9781724026262
ISBN-10: 1724026267
Binding: Paperback or Softback (Trade Paperback (Us))
Content Language: English
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Page Count: 38
Carton Quantity: 108
Product Dimensions: 8.50 x 0.08 x 11.00 inches
Weight: 0.25 pound(s)
Country of Origin: US
Subject Information
BISAC Categories
Science | Space Science - General
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Multi-field mechanics are presented for curvilinear piezoelectric laminates interfaced with distributed passive electric components. The equations of motion for laminated piezoelectric shell structures with embedded passive electric networks are directly formulated and solved using a finite element methodology. The modal damping and frequencies of the piezoelectric shell are calculated from the poles of the system. Experimental and numerical results are presented for the modal damping and frequency of composite beams with a resistively shunted piezoceramic patch. The modal damping and frequency of plates, cylindrical shells and cylindrical composite blades with piezoelectric-resistor layers are predicted. Both analytical and experimental studies illustrate a unique dependence of modal damping and frequencies on the shunting resistance and show the effect of structural shape and curvature on piezoelectric damping. Saravanos, Dimitris A. Glenn Research Center NASA/CR-1999-208871, NAS 1.26:208871, E-11515
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Paperback