LEADER 00926cam0 2200241 450 001 E600200011118 005 20210625100723.0 100 $a20050628d2000 |||||ita|0103 ba 101 $aeng 102 $aGB 200 1 $aMyth and Philosophy from the presocratic to Plato$fKathryna A. Morgan 210 $aCambridge$cCambridge University Press$d2000 215 $aVIII,314 p.$d24 cm 700 1$aMorgan$b, Kathryn A.$3AF00011328$4070$0675123 801 0$aIT$bUNISOB$c20210625$gRICA 850 $aUNISOB 852 $aUNISOB$jFondo|Crie$m126302 912 $aE600200011118 940 $aM 102 Monografia moderna SBN 941 $aM 957 $aFondo|Crie$b000215$gSi$d126302$hCrie$racquisto$1catenacci$2UNISOB$3UNISOB$420050628090431.0$520210625100723.0$6bethb$fPer le modalità di consultazione vedi homepage della Biblioteca link Fondi 996 $aMyth and Philosophy from the presocratic to Plato$91671546 997 $aUNISOB LEADER 01831nam 2200481 450 001 9910707044003321 005 20160324160402.0 035 $a(CKB)5470000002461049 035 $a(OCoLC)945556941 035 $a(EXLCZ)995470000002461049 100 $a20160324j199710 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 13$aAn experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses /$fEdward P. Phillips 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dOctober 1997. 215 $a1 online resource (14 pages) $cillustrations 225 1 $aNASA technical memorandum ;$v4784 300 $aTitle from title screen (viewed March 24, 2016). 300 $a"October 1997." 300 $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page. 320 $aIncludes bibliographical references (page 5). 606 $aCrack propagation$2nasat 606 $aFatigue (materials)$2nasat 606 $aAluminum$2nasat 606 $aBending fatigue$2nasat 606 $aAluminum alloys$2nasat 615 7$aCrack propagation. 615 7$aFatigue (materials) 615 7$aAluminum. 615 7$aBending fatigue. 615 7$aAluminum alloys. 700 $aPhillips$b Edward P.$01412274 712 02$aLangley Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910707044003321 996 $aAn experimental study of fatigue crack growth in aluminum sheet subjected to combined bending and membrane stresses$93505284 997 $aUNINA