LEADER 01625nam  2200469I  450 
001 9910706120703321
005 20170914084516.0
035   $a(CKB)5470000002455223
035   $a(OCoLC)1003640668
035   $a(EXLCZ)995470000002455223
100   $a20170914j199910    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEvaluation of pressurization fatigue life of 1441 Al-Li fuselage panel /$fR. Keith Bird and Dennis L. Dicus
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dOctober 1999.
215   $a1 online resource (22 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209684
300   $a"October 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 6).
606   $aAluminum-lithium alloys$2nasat
606   $aFatigue life$2nasat
606   $aFuselages$2nasat
606   $aMechanical properties$2nasat
606   $aPressurizing$2nasat
615  7$aAluminum-lithium alloys.
615  7$aFatigue life.
615  7$aFuselages.
615  7$aMechanical properties.
615  7$aPressurizing.
700   $aBird$b R. Keith$01409929
702   $aDicus$b Dennis L.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706120703321
996   $aEvaluation of pressurization fatigue life of 1441 Al-Li fuselage panel$93497601
997   $aUNINA