LEADER 01733nam  2200505Ia 450 
001 9910701779403321
005 20120515121630.0
035   $a(CKB)5470000002420301
035   $a(OCoLC)793644818
035   $a(EXLCZ)995470000002420301
100   $a20120515d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aDesign, optimization, and evaluation of integrally-stiffened Al-2139 panel with curved stiffeners$b[electronic resource] /$fDavid Havens ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (43 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2011-217308
300   $aTitle from title screen (viewed on Mar. 15, 2012).
300   $a"November 2011."
320   $aIncludes bibliographical references (page 28).
606   $aDesign optimization$2nasat
606   $aLoad tests$2nasat
606   $aTolerances (mechanics)$2nasat
606   $aPanels$2nasat
606   $aStiffening$2nasat
606   $aCurvature$2nasat
606   $aLoads (forces)$2nasat
615  7$aDesign optimization.
615  7$aLoad tests.
615  7$aTolerances (mechanics)
615  7$aPanels.
615  7$aStiffening.
615  7$aCurvature.
615  7$aLoads (forces)
701   $aHavens$b David$01421577
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701779403321
996   $aDesign, optimization, and evaluation of integrally-stiffened Al-2139 panel with curved stiffeners$93543251
997   $aUNINA