LEADER 01434nam0-2200421---450 001 990005707000203316 005 20190403125007.0 035 $a000570700 035 $aUSA01000570700 035 $a(ALEPH)000570700USA01 035 $a000570700 100 $a20070326d1973----|||y0itaa50------ba 101 $afre 102 $afr 105 $a0 00||| 200 1 $a<> crise contemporaine$edu modernisme à la crise des herméneutiques$fpar Jean Greisch, Karl Neufeld, Christoph Theobald$gavant-propos de C. Kannengiesser 210 $aParis$cBeauchesne$dc1973 215 $a190 p.$d22 cm. 225 2 $aThèologie historique. Etudes$fpubliées par les professeurs de théologie à l'institut catholique de Paris$gsous la direction de Jean Daniélou$v24 410 0$12001$aThèologie historique. Etudes$v24 606 $aTeologia fondamentale$2F 620 $dPARIS 676 $a270.82 700 1$aGREISCH,$bJean$0155397 701 1$aNEUFELD,$bKarl$0549046 701 1$aTHEOBALD,$bChristoph$0615477 702 1$aKANNENGIESSER,$bCharles 801 0$aIT$bSA$c20111219 912 $a990005707000203316 950 0$aDipar.to di Filosofia - Salerno$dDFCC 270.82 GRE$e3071 FIL 951 $aCC 270.82 GRE$b3071 FIL 959 $aBK 969 $aFIL 979 $c20121027$lUSA01$h1526 979 $c20121027$lUSA01$h1615 996 $aCrise contemporaine$91083769 997 $aUNISA NUM $aSA0019514 LEADER 01747nam 2200493I 450 001 9910703786703321 005 20150604153919.0 035 $a(CKB)5470000002433851 035 $a(OCoLC)910680300 035 $a(EXLCZ)995470000002433851 100 $a20150604j201502 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aEnabling rapid and robust structural analysis during conceptual design /$fLloyd B. Eldred, Sharon L. Padula, and Wu Li 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dFebruary 2015. 215 $a1 online resource (21 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2015-218687 300 $aTitle from title screen (viewed June 4, 2015). 300 $a"February 2015." 320 $aIncludes bibliographical references (pages 20-21). 606 $aStructural analysis$2nasat 606 $aAerodynamic loads$2nasat 606 $aSupersonic aircraft$2nasat 606 $aBody-wing configurations$2nasat 606 $aDesign analysis$2nasat 615 7$aStructural analysis. 615 7$aAerodynamic loads. 615 7$aSupersonic aircraft. 615 7$aBody-wing configurations. 615 7$aDesign analysis. 700 $aEldred$b Lloyd B.$01408898 702 $aPadula$b S. L. 702 $aLi$b Wu 712 02$aLangley Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910703786703321 996 $aEnabling rapid and robust structural analysis during conceptual design$93494011 997 $aUNINA