LEADER 01896nam  2200493I  450 
001 9910707942003321
005 20170208091333.0
035   $a(CKB)5470000002469150
035   $a(OCoLC)971615426
035   $a(EXLCZ)995470000002469150
100   $a20170208j201611    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFull-field reconstruction of structural deformations and loads from measured strain data on a wing test article using the inverse finite element method /$fEric J. Miller and Russel Manalo, Alexander Tessler
210  1$aEdwards, California :$cNational Aeronautics and Space Administration, Armstrong Flight Research Center,$dNovember 2016.
215   $a1 online resource (29 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2016-219407
300   $a"November 2016."
320   $aIncludes bibliographical references (pages 28-29).
606   $aAerodynamic loads$2nasat
606   $aBody-wing and tail configurations$2nasat
606   $aDeformation$2nasat
606   $aFinite element method$2nasat
606   $aStrain measurement$2nasat
606   $aWing loading$2nasat
615  7$aAerodynamic loads.
615  7$aBody-wing and tail configurations.
615  7$aDeformation.
615  7$aFinite element method.
615  7$aStrain measurement.
615  7$aWing loading.
700   $aMiller$b Eric J.$0614271
702   $aManalo$b Russel
702   $aTessler$b Alexander
712 02$aNASA Neil A. Armstrong Flight Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707942003321
996   $aFull-field reconstruction of structural deformations and loads from measured strain data on a wing test article using the inverse finite element method$93465795
997   $aUNINA