Validation Of High Displacement Piezoelectric Actuator Finite Element Models

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Validation of High Displacement Piezoelectric Actuator Finite Element Models
Language: en
Pages: 30
Authors: National Aeronautics and Space Adm Nasa
Categories: Science
Type: BOOK - Published: 2018-09-25 - Publisher: Independently Published

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The paper presents the results obtained by using NASTRAN(Registered Trademark) and ANSYS(Regitered Trademark) finite element codes to predict doming of the THUN
Validation of High Displacement Piezoelectric Actuator Finite Element Models
Language: en
Pages: 16
Authors: Barmac K. Taleghani
Categories:
Type: BOOK - Published: 2000 - Publisher:

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Validation of High Displacement Piezoelectric Actuator Finite Element Models
Language: en
Pages: 24
Authors: Barmac K. Taleghani
Categories: ANSYS (Computer system)
Type: BOOK - Published: 2000 - Publisher:

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The paper presents the results obtained by using NASTRAN® and ANSYS® finite element codes to predict doming of the THUNDER piezoelectric actuators during the
Nonlinear Geometric Response of Structure with Piezoelectric Actuator by Reduced Order Modeling Using a Temperature Analogy
Language: en
Pages: 44
Authors: Varun Vyas
Categories: Actuators
Type: BOOK - Published: 2014 - Publisher:

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The focus of this investigation is on the formulation and a validation of reduced order models (ROMs) for the prediction of the response of structures with embe
Non-Linear Finite Element Modeling of Thunder Piezoelectric Actuators
Language: en
Pages: 32
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-06-15 - Publisher: Createspace Independent Publishing Platform

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A NASTRAN non-linear finite element model has been developed for predicting the dome heights of THUNDER (THin Layer UNimorph Ferroelectric DrivER) piezoelectric