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001 9910706220203321
005 20171030152709.0
035   $a(CKB)5470000002456238
035   $a(OCoLC)1008595885
035   $a(EXLCZ)995470000002456238
100   $a20171030j200004    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAdvances in fatigue and fracture mechanics analyses for metallic aircraft structures /$fJ.C. Newman, Jr
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2000.
215   $a1 online resource (40 pages) $cillustrations
225 1 $aNASA/TM ;$v2000-210084
300   $a"April 2000."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 19-24).
606   $aAircraft structures$2nasat
606   $aCracks$2nasat
606   $aFinite element method$2nasat
606   $aFracture mechanics$2nasat
606   $aStress analysis$2nasat
606   $aMetals$2nasat
606   $aCrack propagation$2nasat
606   $aMetal fatigue$2nasat
615  7$aAircraft structures.
615  7$aCracks.
615  7$aFinite element method.
615  7$aFracture mechanics.
615  7$aStress analysis.
615  7$aMetals.
615  7$aCrack propagation.
615  7$aMetal fatigue.
700   $aNewman$b J. C.$0878389
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706220203321
996   $aAdvances in fatigue and fracture mechanics analyses for metallic aircraft structures$93454909
997   $aUNINA