LEADER 01016nam--2200361---450- 001 990001927890203316 005 20050114135406.0 035 $a000192789 035 $aUSA01000192789 035 $a(ALEPH)000192789USA01 035 $a000192789 100 $a20040812d1911----km-y0itay0103----ba 101 0 $aita 102 $aIT 105 $a||||||||001yy 200 1 $a<> prose$fPercy Bysshe Shelley$gtrad. di F. M. Martini 210 $aRoma$cVorghera$d1911 215 $a245 p.$d22 cm 225 $aAutori celebri stranieri$v14 410 0 $12001$aAutori celebri stranieri$v14 410 0$12001 454 1$12001 461 1$1001-------$12001 700 1$aSHELLEY,$bPercy Bysshe$0167778 801 0$aIT$bsalbc$gSBD 912 $a990001927890203316 951 $aVII.3.A. 83(Varie Coll 137/14)$b447797 L.M.$cVarie Coll 959 $aBK 969 $aUMA 979 $aSIAV7$b10$c20040812$lUSA01$h1321 979 $aCOPAT3$b90$c20050114$lUSA01$h1354 996 $aProse$991852 997 $aUNISA LEADER 01935nam 2200529Ia 450 001 9910701781203321 005 20120531135115.0 035 $a(CKB)5470000002420283 035 $a(OCoLC)794557657 035 $a(EXLCZ)995470000002420283 100 $a20120531d2011 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aDevelopment and application of benchmark examples for mode II static delamination propagation and fatigue growth predictions$b[electronic resource] /$fRonald Krueger 210 1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center :$cNational Institute of Aerospace,$d[2011] 215 $a1 online resource (68 pages) $ccolor illustrations 225 1 $a[NASA contractor report] ;$vNASA/CR-2011-217305 300 $aTitle from title screen (viewed on May 31, 2012). 300 $a"November 2011." 300 $a"NIA report no. 2011-02." 320 $aIncludes bibliographical references. 606 $aDelaminating$2nasat 606 $aMathematical models$2nasat 606 $aFatigue (materials)$2nasat 606 $aFlexing$2nasat 606 $aCrack closure$2nasat 606 $aStress propagation$2nasat 606 $aStatic loads$2nasat 615 7$aDelaminating. 615 7$aMathematical models. 615 7$aFatigue (materials) 615 7$aFlexing. 615 7$aCrack closure. 615 7$aStress propagation. 615 7$aStatic loads. 700 $aKrueger$b Ronald$01395935 712 02$aLangley Research Center. 712 02$aNational Institute of Aerospace. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910701781203321 996 $aDevelopment and application of benchmark examples for mode II static delamination propagation and fatigue growth predictions$93467746 997 $aUNINA