LEADER 02055nam  2200541   450 
001 9910707862103321
005 20161214101809.0
035   $a(CKB)5470000002467936
035   $a(OCoLC)965907409
035   $a(EXLCZ)995470000002467936
100   $a20161214j199607    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCorrelation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box /$fJohn T. Wang [and three others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJuly 1996.
215   $a1 online resource (33 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110267
300   $a"July 1996."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (pages 13-14).
517 3 $aCorrelation of structural analysis and test results for the McDonnell Douglas stitched resin film infusion all-composite wing stub box
606   $aComposite structures$2nasat
606   $aFinite element method$2nasat
606   $aGraphite-epoxy composites$2nasat
606   $aWings$2nasat
606   $aStrain distribution$2nasat
606   $aBending$2nasat
606   $aCommercial aircraft$2nasat
606   $aAircraft structures$2nasat
615  7$aComposite structures.
615  7$aFinite element method.
615  7$aGraphite-epoxy composites.
615  7$aWings.
615  7$aStrain distribution.
615  7$aBending.
615  7$aCommercial aircraft.
615  7$aAircraft structures.
700   $aWang$b John T.$01415896
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707862103321
996   $aCorrelation of structural analysis and test results for the McDonnell Douglas stitched$93519364
997   $aUNINA