LEADER 01891nam  2200553Ia 450 
001 9910701449703321
005 20120308152323.0
035   $a(CKB)5470000002418581
035   $a(OCoLC)779542128
035   $a(EXLCZ)995470000002418581
100   $a20120308d2011      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aDesign, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners$b[electronic resource] /$fWesley C.H. Slemp ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (39 pages) $cillustrations (some color)
225 1 $aNASA/TP ;$v2011-217178
300   $aTitle from title screen (viewed on Mar. 8, 2012).
300   $a"September 2011."
320   $aIncludes bibliographical references (pages 22-23).
606   $aBuckling$2nasat
606   $aFinite element method$2nasat
606   $aDesign optimization$2nasat
606   $aLoad tests$2nasat
606   $aElastic buckling$2nasat
606   $aWing panels$2nasat
606   $aFixtures$2nasat
606   $aDeflection$2nasat
606   $aLoads (forces)$2nasat
615  7$aBuckling.
615  7$aFinite element method.
615  7$aDesign optimization.
615  7$aLoad tests.
615  7$aElastic buckling.
615  7$aWing panels.
615  7$aFixtures.
615  7$aDeflection.
615  7$aLoads (forces)
701   $aSlemp$b Wesley C. H$01407850
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701449703321
996   $aDesign, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners$93490282
997   $aUNINA