LEADER 01797nam  2200517I  450 
001 9910702110303321
005 20130130163408.0
035   $a(CKB)5470000002425039
035   $a(OCoLC)826035564
035   $a(EXLCZ)995470000002425039
100   $a20130130d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aImplementation of a smeared crack band model in a micromechanics framework /$fEvan J. Pineda [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (52 pages) $ccolor illustrations
225 1 $a[NASA technical memorandum] ;$vNASA/TM 2012-217603
300   $aTitle from title screen (viewed Jan. 30, 2013).
300   $a"June 2012."
320   $aIncludes bibliographical references (page 50-52).
606   $aCracks$2nasat
606   $aMicromechanics$2nasat
606   $aMathematical models$2nasat
606   $aSmear$2nasat
606   $aMechanical properties$2nasat
606   $aFracture mechanics$2nasat
606   $aFiber composites$2nasat
615  7$aCracks.
615  7$aMicromechanics.
615  7$aMathematical models.
615  7$aSmear.
615  7$aMechanical properties.
615  7$aFracture mechanics.
615  7$aFiber composites.
700   $aPineda$b Evan J.$01387412
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702110303321
996   $aImplementation of a smeared crack band model in a micromechanics framework$93492464
997   $aUNINA