LEADER 01818nam  2200505Ia 450 
001 9910700303703321
005 20110628145152.0
035   $a(CKB)5470000002409955
035   $a(OCoLC)733349754
035   $a(EXLCZ)995470000002409955
100   $a20110628d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPre-test analysis predictions for the shell buckling knockdown factor checkout tests, TA01 and TA02$b[electronic resource] /$fRobert P. Thornburgh, Mark W. Hilburger
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (vii, 37 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2011-216875
300   $aTitle from title screen (viewed on June 28, 2011).
300   $a"January 2011."
300   $a"ARL-TR-5123."
320   $aIncludes bibliographical references (page 37).
606   $aStructural analysis$2nasat
606   $aLithium alloys$2nasat
606   $aShell stability$2nasat
606   $aCylindrical shells$2nasat
606   $aAluminum alloys$2nasat
606   $aLoads (forces)$2nasat
615  7$aStructural analysis.
615  7$aLithium alloys.
615  7$aShell stability.
615  7$aCylindrical shells.
615  7$aAluminum alloys.
615  7$aLoads (forces)
700   $aThornburgh$b Robert P$01406545
701   $aHilburger$b Mark W$g(Mark William)$01395062
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700303703321
996   $aPre-test analysis predictions for the shell buckling knockdown factor checkout tests, TA01 and TA02$93485819
997   $aUNINA