LEADER 01858nam  2200541I  450 
001 9910702505603321
005 20140930112528.0
035   $a(CKB)5470000002429127
035   $a(OCoLC)891566928
035   $a(EXLCZ)995470000002429127
100   $a20140929j201405    ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMitigation of crack damage in metallic materials /$fPatrick Leser [and seven others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 2014.
215   $a1 online resource (17 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2014-218272
300   $aTitle from title screen (viewed Sept. 29, 2014).
300   $a"May 2014."
320   $aIncludes bibliographical references (pages 12-13).
606   $aFatigue (materials)$2nasat
606   $aTolerances (mechanics)$2nasat
606   $aCrack opening displacement$2nasat
606   $aMetal fatigue$2nasat
606   $aCrack closure$2nasat
606   $aCrack propagation$2nasat
606   $aTitanium alloys$2nasat
606   $aAerospace vehicles$2nasat
615  7$aFatigue (materials)
615  7$aTolerances (mechanics)
615  7$aCrack opening displacement.
615  7$aMetal fatigue.
615  7$aCrack closure.
615  7$aCrack propagation.
615  7$aTitanium alloys.
615  7$aAerospace vehicles.
700   $aLeser$b Patrick E.$01423051
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702505603321
996   $aMitigation of crack damage in metallic materials$93549255
997   $aUNINA