LEADER 01711nam 22005653 450 001 9910133587203321 005 20130711124415.0 010 $a88-95844-82-3 035 $a(CKB)3280000000014300 035 $a(ItFiC)it 02567829 035 $a(SSID)ssj0000857367 035 $a(PQKBManifestationID)12400557 035 $a(PQKBTitleCode)TC0000857367 035 $a(PQKBWorkID)10856442 035 $a(PQKB)10354979 035 $a(EXLCZ)993280000000014300 100 $a20130405d2012 uy 0 101 0 $aita 181 $ctxt 182 $cc 183 $acr 200 10$aDalle parti di Aldo $evicende e protagonisti della cultura tipografica italiana del Novecento /$fMassimo Gatta ; a cura di Dionigi Colnaghi ; prefazione di Edoardo Barbieri ; con uno scritto di Mauro Chiabrando 210 $aMacerata $cBiblohaus$d2012 215 $a440 p 300 $aBibliographic Level Mode of Issuance: Monograph 311 $a88-95844-24-6 517 $aDalle parti di Aldo 606 $aPrinting$zItaly$xHistory 606 $aPrinters$zItaly 606 $aPrinting$xHistory$zItaly 606 $aPrinters$zItaly 606 $aEducation$2HILCC 606 $aSocial Sciences$2HILCC 606 $aBook Studies & Arts$2HILCC 615 0$aPrinting$xHistory. 615 0$aPrinters 615 0$aPrinting$xHistory 615 0$aPrinters 615 7$aEducation 615 7$aSocial Sciences 615 7$aBook Studies & Arts 676 $a686 700 $aGatta$b Massimo$0501026 702 $aColnaghi$b Dionigi 801 0$bItFiC 801 1$bItFiC 906 $aBOOK 912 $a9910133587203321 996 $aDalle parti di Aldo$92430851 997 $aUNINA LEADER 01753nam 2200493 450 001 9910704816303321 005 20140212082156.0 035 $a(CKB)5470000002445576 035 $a(OCoLC)870332862 035 $a(EXLCZ)995470000002445576 100 $a20140212d2013 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 13$aAn Approximate solution and master curves for buckling of symmetrically laminated composite cylinders /$fMichael P. Nemeth 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$d2013. 215 $a1 online resource (60 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2013-217999 300 $aTitle from title screen (viewed on Feb. 12, 2014). 300 $a"May 2013." 320 $aIncludes bibliographical references (page 19). 606 $aAnisotropy$2nasat 606 $aAxial compression loads$2nasat 606 $aCylindrical shells$2nasat 606 $aInhomogeneity$2nasat 606 $aLaminates$2nasat 606 $aSandwich structures$2nasat 615 7$aAnisotropy. 615 7$aAxial compression loads. 615 7$aCylindrical shells. 615 7$aInhomogeneity. 615 7$aLaminates. 615 7$aSandwich structures. 700 $aNemeth$b Michael P.$01391721 712 02$aLangley Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910704816303321 996 $aAn Approximate solution and master curves for buckling of symmetrically laminated composite cylinders$93514065 997 $aUNINA