LEADER 01473oam  2200469I  450 
001 9910691729003321
005 20171222125845.0
035   $a(CKB)5470000002348106
035   $a(OCoLC)1016454983
035   $a(EXLCZ)995470000002348106
100   $a20171222j200104    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStructural testing of a stitched/resin film infused graphite-epoxy wing box /$fDawn C. Jegley and Harold G. Bush
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2001.
215   $a1 online resource (i, 116 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210846
300   $a"April 2001."
320   $aIncludes bibliographical references (page 16).
606   $aGraphite-epoxy composites$2nasat
606   $aWings$2nasat
606   $aImpact damage$2nasat
606   $aBending$2nasat
606   $aFailure$2nasat
615  7$aGraphite-epoxy composites.
615  7$aWings.
615  7$aImpact damage.
615  7$aBending.
615  7$aFailure.
700   $aJegley$b Dawn C.$01395474
702   $aBush$b Harold G.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910691729003321
996   $aStructural testing of a stitched$93456305
997   $aUNINA