LEADER 00946nam0-2200301---450- 001 990008785300403321 005 20090123124817.0 035 $a000878530 035 $aFED01000878530 035 $a(Aleph)000878530FED01 035 $a000878530 100 $a20081223d1929----km-y0itay50------ba 101 0 $afre 102 $aCH 105 $af-------001yy 200 1 $aSur une méthode d'analyse qualitative rapide des cations et anions les plus usuels$fthèse par Grégoire Gutzeit 210 $aBâle$cImprimerie E. Birkhaeuser$d1929 215 $a56 p., tav.$d24 cm 610 0 $aAnalisi qualitativa 676 $a544$v20$zita 700 1$aGutzeit,$bGrégoire$0431216 801 0$aIT$bUNINA$gRICA$2UNIMARC 901 $aBK 912 $a990008785300403321 952 $a60 MISC. B 226/16$fFAGBC 959 $aFAGBC 996 $aSur une méthode d'analyse qualitative rapide des cations et anions les plus usuels$9809359 997 $aUNINA LEADER 01889nam 2200553 450 001 9910706191003321 005 20170817142744.0 035 $a(CKB)5470000002454513 035 $a(OCoLC)1001296703 035 $a(EXLCZ)995470000002454513 100 $a20170817j199812 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aMethodology for predicting the onset of widespread fatigue damage in lap-splice joints /$fJ.C. Newman, Jr. [and three others] 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1998. 215 $a1 online resource (15 pages) $cillustrations 225 1 $aNASA/TM ;$v1998-208975 300 $a"December 1998." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (pages 10-11). 606 $aCrack propagation$2nasat 606 $aCrack tips$2nasat 606 $aAirframes$2nasat 606 $aStress analysis$2nasat 606 $aLap joints$2nasat 606 $aFuselages$2nasat 606 $aFinite element method$2nasat 606 $aFatigue tests$2nasat 606 $aFatigue (materials)$2nasat 615 7$aCrack propagation. 615 7$aCrack tips. 615 7$aAirframes. 615 7$aStress analysis. 615 7$aLap joints. 615 7$aFuselages. 615 7$aFinite element method. 615 7$aFatigue tests. 615 7$aFatigue (materials) 700 $aNewman$b J. C.$0878389 712 02$aLangley Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910706191003321 996 $aMethodology for predicting the onset of widespread fatigue damage in lap-splice joints$93497635 997 $aUNINA