01896nam 2200493I 450 991070794200332120170208091333.0(CKB)5470000002469150(OCoLC)971615426(EXLCZ)99547000000246915020170208j201611 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierFull-field reconstruction of structural deformations and loads from measured strain data on a wing test article using the inverse finite element method /Eric J. Miller and Russel Manalo, Alexander TesslerEdwards, California :National Aeronautics and Space Administration, Armstrong Flight Research Center,November 2016.1 online resource (29 pages) color illustrationsNASA/TM ;2016-219407"November 2016."Includes bibliographical references (pages 28-29).Aerodynamic loadsnasatBody-wing and tail configurationsnasatDeformationnasatFinite element methodnasatStrain measurementnasatWing loadingnasatAerodynamic loads.Body-wing and tail configurations.Deformation.Finite element method.Strain measurement.Wing loading.Miller Eric J.614271Manalo RusselTessler AlexanderNASA Neil A. Armstrong Flight Research Center,GPOGPOBOOK9910707942003321Full-field reconstruction of structural deformations and loads from measured strain data on a wing test article using the inverse finite element method3465795UNINA