LEADER 01914nam 2200505Ia 450 001 9910699254303321 005 20230902162200.0 035 $a(CKB)5470000002401363 035 $a(OCoLC)476753730 035 $a(EXLCZ)995470000002401363 100 $a20091210d1985 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aThree-dimensional elastic-plastic finite-element analysis of fatigue crack propagation$b[electronic resource] /$fby R.G. Chermahini and G.L. Goglia 210 1$aNorfolk, Va. :$cOld Dominion University Research Foundation,$d[1985] 215 $a1 volume $cPDF file 300 $aTitle from title screen (viewed Dec. 3, 2009). 300 $a"Final report for the period June 1, 1985 to November 1, 1985." 300 $a"Prepared for National Aeronautics and Space Administration Langley Research Center, under Research Grant NAG-1-529." 300 $a"November 1985." 320 $aIncludes bibliographical references. 410 0$aNASA contractor report ;$vNASA CR-176415. 606 $aAircraft structures$2nasat 606 $aCrack propagation$2nasat 606 $aCracks$2nasat 606 $aFatigue (materials)$2nasat 606 $aFinite element method$2nasat 615 7$aAircraft structures. 615 7$aCrack propagation. 615 7$aCracks. 615 7$aFatigue (materials) 615 7$aFinite element method. 700 $aChermahini$b R. G$01406412 701 $aGoglia$b G. L$01406413 712 02$aOld Dominion University.$bDepartment of Mechanical Engineering and Mechanics. 712 02$aLangley Research Center. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910699254303321 996 $aThree-dimensional elastic-plastic finite-element analysis of fatigue crack propagation$93485348 997 $aUNINA