LEADER 01153nam2-2200373li-450 001 990000104920203316 005 20170914112051.0 035 $a0010492 035 $aUSA010010492 035 $a(ALEPH)000010492USA01 035 $a0010492 100 $a2001990051966-------y0itay0103----ba 101 0 $aeng 102 $aGB 200 1 $a<>$fG. H. Hardy$gedited by acommittee appointed by the London Mathematical Society 210 $aOxford$cClarendon Press$d1966 215 $a700 p.$c1 ritr.$d26 cm 461 0$10010010493$12001$aCollected papers of G. H. Hardy$v1 700 1$aHARDY,$bGodfrey H.$056528 712 1$aLondon Mathematical Society 801 $aIt$bsalbc$gISBD 912 $a990000104920203316 951 $a510 HAR 1$b6900/CBS$c510$d00328963 959 $aBK 969 $aSCI 979 $c19900517 979 $c20001110$lUSA01$h1710 979 $c20020403$lUSA01$h1618 979 $aPATRY$b90$c20040406$lUSA01$h1608 979 $aRSIAV6$b90$c20091016$lUSA01$h1610 979 $aRSIAV6$b90$c20091016$lUSA01$h1611 979 $aRSIAV6$b90$c20091016$lUSA01$h1612 996 $aVol. 1:$91476043 997 $aUNISA LEADER 01802nam 2200529 450 001 9910706220203321 005 20171030152709.0 035 $a(CKB)5470000002456238 035 $a(OCoLC)1008595885 035 $a(EXLCZ)995470000002456238 100 $a20171030j200004 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAdvances in fatigue and fracture mechanics analyses for metallic aircraft structures /$fJ.C. Newman, Jr 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dApril 2000. 215 $a1 online resource (40 pages) $cillustrations 225 1 $aNASA/TM ;$v2000-210084 300 $a"April 2000." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (pages 19-24). 606 $aAircraft structures$2nasat 606 $aCracks$2nasat 606 $aFinite element method$2nasat 606 $aFracture mechanics$2nasat 606 $aStress analysis$2nasat 606 $aMetals$2nasat 606 $aCrack propagation$2nasat 606 $aMetal fatigue$2nasat 615 7$aAircraft structures. 615 7$aCracks. 615 7$aFinite element method. 615 7$aFracture mechanics. 615 7$aStress analysis. 615 7$aMetals. 615 7$aCrack propagation. 615 7$aMetal fatigue. 700 $aNewman$b J. C.$0878389 712 02$aLangley Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910706220203321 996 $aAdvances in fatigue and fracture mechanics analyses for metallic aircraft structures$93454909 997 $aUNINA