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100   $a20130912j199905    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNon-linear finite element modeling of THUNDER piezoelectric actuators /$fBarmac K. Taleghani, Joel F. Campbell
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center ;$aAlexandria, Virginia :$cU.S. Army Materiel Command,$dMay 1999.
215   $a1 online resource (13 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209322
225 1 $aU. S. Army Research Laboratory technical report ;$vARL-TR-1977
300   $a"May 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 6).
517 3 $aNon-linear finite element modeling of THin Layer UNimorph Ferroelectric DrivER piezoelectric actuators
606   $aFinite element method$2nasat
606   $aMathematical models$2nasat
606   $aPiezoelectricity$2nasat
606   $aActuators$2nasat
606   $aAircraft design$2nasat
615  7$aFinite element method.
615  7$aMathematical models.
615  7$aPiezoelectricity.
615  7$aActuators.
615  7$aAircraft design.
700   $aTaleghani$b Barmac K.$01403198
702   $aCampbell$b Joel F.
712 02$aLangley Research Center,
712 02$aUnited States.$bArmy Materiel Command.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910706170403321
996   $aNon-linear finite element modeling of THUNDER piezoelectric actuators$93475348
997   $aUNINA