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005 20160428141259.0
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035   $a(EXLCZ)995470000002437494
100   $a20160428j201508    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBuckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01 $etest dates: 19-21 November 2008 /$fMark W. Hilburger, W. Allen Waters, Jr., Waddy T. Haynie
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dAugust 2015.
215   $a1 online resource (viii, 61 pages) $ccolor illustrations
225 1 $aNASA/TP ;$v2015-218785
300   $aTitle from title screen (viewed on April 28, 2016).
300   $a"August 2015."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (page 49).
517   $aBuckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01 
606   $aBuckling$2nasat
606   $aAxial strain$2nasat
606   $aCritical loading$2nasat
606   $aPerformance tests$2nasat
606   $aStructural analysis$2nasat
615  7$aBuckling.
615  7$aAxial strain.
615  7$aCritical loading.
615  7$aPerformance tests.
615  7$aStructural analysis.
700   $aHilburger$b Mark W$g(Mark William),$01395062
702   $aWaters$b W. Allen
702   $aHaynie$b Waddy T.
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704016403321
996   $aBuckling test results from the 8-foot-diameter orthogrid-stiffened cylinder test article TA01$93486215
997   $aUNINA