02055nam 2200541 450 991070786210332120161214101809.0(CKB)5470000002467936(OCoLC)965907409(EXLCZ)99547000000246793620161214j199607 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierCorrelation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box /John T. Wang [and three others]Hampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,July 1996.1 online resource (33 pages) illustrationsNASA technical memorandum ;110267"July 1996.""Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (pages 13-14).Correlation of structural analysis and test results for the McDonnell Douglas stitched resin film infusion all-composite wing stub boxComposite structuresnasatFinite element methodnasatGraphite-epoxy compositesnasatWingsnasatStrain distributionnasatBendingnasatCommercial aircraftnasatAircraft structuresnasatComposite structures.Finite element method.Graphite-epoxy composites.Wings.Strain distribution.Bending.Commercial aircraft.Aircraft structures.Wang John T.1415896Langley Research Center,GPOGPOBOOK9910707862103321Correlation of structural analysis and test results for the McDonnell Douglas stitched3519364UNINA