LEADER 00902nam0-2200289 --450 001 9910265660403321 005 20180419134316.0 010 $a978-88-98264-05-6 100 $a20180419d2014----kmuy0itay5050 ba 101 1 $aita$cfre 102 $aIT 105 $ay 001yy 200 1 $a<>Cristianesimo e la cremazione$fPiotr Kuberski$gprefazione di François Bcespflug$gtraduzione dal farncese di Giuseppe Piccinno 210 $aNapoli$cEDI$d2014 215 $a463 p.$d21 cm 610 $aCremazione$aCristianesimo$aLegittimita 676 $a264.020985$v21 700 1$aKuberski,$bPiotr$0749955 702 1$aBcespflug,$bFrancois 702 1$aPiccinno,$bGiuseppe 801 0$aIT$bUNINA$gREICAT$2UNIMARC 901 $aBK 912 $a9910265660403321 952 $a264 KUB 1$bBIBL. 2018/188$fFLFBC 959 $aFLFBC 996 $aCristianesimo e la cremazione$91509338 997 $aUNINA LEADER 01713nam 2200505Ia 450 001 9910701571603321 005 20120328094218.0 035 $a(CKB)5470000002419370 035 $a(OCoLC)781850192 035 $a(EXLCZ)995470000002419370 100 $a20120328d2011 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aReliability based design for a raked wing tip of an airframe$b[electronic resource] /$fSurya N. Patnaik, Shantaram S. Pai and Rula M. Coroneos 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2011] 215 $a1 online resource (16 pages) $cillustrations (some color) 225 1 $aNASA/TM ;$v2011-216808 300 $aTitle from title screen (viewed on Mar. 27, 2012). 300 $a"November 2011." 320 $aIncludes bibliographical references (pages 15-16). 606 $aComposite materials$2nasat 606 $aAirframes$2nasat 606 $aWings$2nasat 606 $aDesign analysis$2nasat 606 $aLoads (forces)$2nasat 606 $aReliability$2nasat 615 7$aComposite materials. 615 7$aAirframes. 615 7$aWings. 615 7$aDesign analysis. 615 7$aLoads (forces) 615 7$aReliability. 700 $aPatnaik$b Surya N$0471368 701 $aPai$b Shantaram S$01407131 701 $aCoroneos$b Rula M$01392718 712 02$aNASA Glenn Research Center. 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910701571603321 996 $aReliability based design for a raked wing tip of an airframe$93487696 997 $aUNINA