02072oam 2200577 450 991070617040332120170825104542.0(CKB)5470000002454721(OCoLC)858280545(EXLCZ)99547000000245472120130912j199905 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierNon-linear finite element modeling of THUNDER piezoelectric actuators /Barmac K. Taleghani, Joel F. CampbellHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center ;Alexandria, Virginia :U.S. Army Materiel Command,May 1999.1 online resource (13 pages) illustrationsNASA/TM ;1999-209322U. S. Army Research Laboratory technical report ;ARL-TR-1977"May 1999.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 6).Non-linear finite element modeling of THin Layer UNimorph Ferroelectric DrivER piezoelectric actuatorsFinite element methodnasatMathematical modelsnasatPiezoelectricitynasatActuatorsnasatAircraft designnasatFinite element method.Mathematical models.Piezoelectricity.Actuators.Aircraft design.Taleghani Barmac K.1403198Campbell Joel F.Langley Research Center,United States.Army Materiel Command.OCLCEOCLCEOCLCOOCLCFOCLCQOCLCOOCLCQGPOBOOK9910706170403321Non-linear finite element modeling of THUNDER piezoelectric actuators3475348UNINA