LEADER 01612nam  2200457I  450 
001 9910702419603321
005 20140724155301.0
035   $a(CKB)5470000002427976
035   $a(OCoLC)884519246
035   $a(EXLCZ)995470000002427976
100   $a20140724d2013      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEvaluation of the behavior of Technova Corporation rod-stiffened stitched compression specimens /$fDawn C. Jegley
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$d2013.
215   $a1 online resource (21 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-218049
300   $aTitle from title screen (viewed on July 24, 2014).
300   $a"October 2013."
606   $aAxial stress$2nasat
606   $aCompression loads$2nasat
606   $aCompressive strength$2nasat
606   $aEpoxy matrix composites$2nasat
606   $aPultrusion$2nasat
615  7$aAxial stress.
615  7$aCompression loads.
615  7$aCompressive strength.
615  7$aEpoxy matrix composites.
615  7$aPultrusion.
700   $aDawn C. Jegley$01423223
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702419603321
996   $aEvaluation of the behavior of Technova Corporation rod-stiffened stitched compression specimens$93550083
997   $aUNINA