01678nam 2200457I 450 991070624930332120171018083920.0(CKB)5470000002455945(OCoLC)1006639218(EXLCZ)99547000000245594520171018j201604 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierFinite element analysis and test results comparison for the hybrid wing body center section test article /Adam Przekop [and three others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,April 2016.1 online resource (viii, 106 pages) color illustrationsNASA/TM ;2016-218973"April 2016.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 104-105).Critical loadingnasatFinite element methodnasatStrain measurementnasatStructural stabilitynasatWingsnasatCritical loading.Finite element method.Strain measurement.Structural stability.Wings.Przekop Adam1393174Langley Research Center,GPOGPOBOOK9910706249303321Finite element analysis and test results comparison for the hybrid wing body center section test article3448981UNINA