LEADER 01770nam  2200505Ia 450 
001 9910702210403321
005 20121113143249.0
035   $a(CKB)5470000002426049
035   $a(OCoLC)817725601
035   $a(EXLCZ)995470000002426049
100   $a20121113d2012      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 00$aDesign, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners$b[electronic resource] /$fSameer B. Mulani ... [and others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2012]
215   $a1 online resource (x, 33 pages) $cillustrations (some color)
225 1 $aNASA/TP ;$v2012-217584
300   $aTitle from title screen (viewed on Nov. 13, 2012).
300   $a"June 2012."
320   $aIncludes bibliographical references (pages 20-22).
606   $aDesign optimization$2nasat
606   $aFinite element method$2nasat
606   $aPhotogrammetry$2nasat
606   $aAluminum alloys$2nasat
606   $aDigital systems$2nasat
606   $aDisplacement$2nasat
606   $aBuckling$2nasat
615  7$aDesign optimization.
615  7$aFinite element method.
615  7$aPhotogrammetry.
615  7$aAluminum alloys.
615  7$aDigital systems.
615  7$aDisplacement.
615  7$aBuckling.
701   $aMulani$b Sameer B$01417407
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702210403321
996   $aDesign, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners$93525673
997   $aUNINA