LEADER 01743oam  2200469 a 450 
001 9910701830503321
005 20120615135048.0
035   $a(CKB)5470000002421805
035   $a(OCoLC)795582847
035   $a(EXLCZ)995470000002421805
100   $a20120615d1986      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFatigue crack growth under general-yielding cyclic-loading$b[electronic resource] /$fZheng Minzhong and H.W. Liu
210  1$aSyracuse, N.Y. :$cSyracuse University, Dept. of Mechanical and Aerospace Engineering ;$a[Cleveland, Ohio] :$cNational Aeronautics and Space Administration, Lewis Research Center,$d[1986]
215   $a1 online resource (i, 25 pages) $cillustrations
225 1 $aNASA contractor report ;$v175049
300   $aTitle from title screen (viewed on June 15, 2012).
300   $a"February 1986."
320   $aIncludes bibliographical references (pages 11-13).
606   $aCrack initiation$2nasat
606   $aCrack propagation$2nasat
606   $aCyclic loads$2nasat
606   $aFatigue (materials)$2nasat
615  7$aCrack initiation.
615  7$aCrack propagation.
615  7$aCyclic loads.
615  7$aFatigue (materials)
700   $aMinzhong$b Zheng$01407855
701   $aLiu$b H. W$g(Hao Wen),$f1926-$01393223
712 02$aSyracuse University.$bDepartment of Mechanical and Aerospace Engineering.
712 02$aLewis Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910701830503321
996   $aFatigue crack growth under general-yielding cyclic-loading$93490309
997   $aUNINA