LEADER 01391oam 2200433zu 450 001 9910164726003321 005 20210807002216.0 010 $a0-8031-4595-0 035 $a(CKB)3170000000044840 035 $a(SSID)ssj0001489673 035 $a(PQKBManifestationID)11823804 035 $a(PQKBTitleCode)TC0001489673 035 $a(PQKBWorkID)11459349 035 $a(PQKB)11473914 035 $a(NjHacI)993170000000044840 035 $a(EXLCZ)993170000000044840 100 $a20160829d1971 uy 101 0 $aeng 135 $aur||||||||||| 181 $ctxt 182 $cc 183 $acr 200 10$aDamage Tolerance in Aircraft Structures 210 31$a[Place of publication not identified]$cAmerican Society for Testing & Materials$d1971 215 $a1 online resource (viii, 251 pages) $cillustrations 225 1 $aASTM special technical publication ;$v486 300 $aBibliographic Level Mode of Issuance: Monograph 311 $a0-8031-0031-0 320 $aIncludes bibliographical references and index. 410 0$aASTM special technical publication ;$v486. 606 $aAirframes$xFatigue 615 0$aAirframes$xFatigue. 676 $a629.13431 700 $aRosenfeld$b M. S$0946510 801 0$bPQKB 906 $aBOOK 912 $a9910164726003321 996 $aDamage Tolerance in Aircraft Structures$92232608 997 $aUNINA