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dc.contributor.authorLazarus, Kenneth B.en_US
dc.contributor.authorCrawley, Edward F.en_US
dc.contributor.otherMassachusetts Institute of Technology. Gas Turbine Laboratoryen_US
dc.date.accessioned2016-10-06T21:22:18Z
dc.date.available2016-10-06T21:22:18Z
dc.date.issued1989en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/104737
dc.descriptionMarch 1989en_US
dc.descriptionOriginally written by Mr. Lazarus as: Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989en_US
dc.descriptionIncludes bibliographical references (pages 126-128)en_US
dc.description.abstractTwo models of induced strain plate actuator/substrate systems are developed and verified experimentally. Equations relating the actuation strains produced by the strain actuators to the induced strains found in the system are derived for both models. In addition, the plate strain energy relations are also developed. Exact and approximate solutions are formulated for isotropic and anisotropic plate systems. Exact solutions are found for actuator/substrate systems with free-free, free-free boundary conditions, and a general procedure for solving the strain energy equations with a Rayleigh-Ritz approximate solution is formulated for systems with arbitrary boundary conditions and external loads. Specific solutions are detailed for cantilever plate systems, including a discussion of the assumed modes selected. A model for predicting the actuation strains produced by a specific class of induced strain actuators, piezoceramic actuators, is also developed.en_US
dc.description.abstractThe non-linear properties of piezoceramics are discussed and the important effects of such non-linearities are accounted for by developing a strain dependent model for the actuation strains created in piezoceramics. The models developed were verified through experimentation via two sets of plate test articles. The first set of simple test articles were used to verify the accuracy of the basic induced strain actuation models, the strain dependence of piezoceramic actuation strains, and a semi-empirical solution procedure. The second, more representative, set of large cantilever plate test articles verified the ability of the models to predict the strains induced in systems with extensive stiffness couplings and complicated boundary conditions, and the Ritz model.en_US
dc.description.abstractAgreement between the solutions predicted by the induced strain actuator models and the experimentally measured deformations was excellent, verifying the effectiveness of using induced strain actuation for shape control of structures such as aeroelastic lifting surfaces and components of intelligent structures.en_US
dc.description.sponsorshipSponsored by General Dynamics Corporation and the Allison Gas Turbine division of General Motors Corporationen_US
dc.format.extent128 pagesen_US
dc.publisherCambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1989]en_US
dc.relation.ispartofseriesGTL report #197en_US
dc.subject.lccTJ778.M41 G24 no.197en_US
dc.subject.lcshActuatorsen_US
dc.subject.lcshStrains and stressesen_US
dc.subject.lcshDeformations (Mechanics)en_US
dc.titleInduced strain actuation of composite platesen_US
dc.title.alternativeComposite plates, Induced strain actuation ofen_US
dc.typeTechnical Reporten_US
dc.identifier.oclc21504011en_US


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