LEADER 00974cam0-2200337---450 001 990009327110403321 005 20181004140157.0 010 $a978-88-498-2853-5 035 $a000932711 035 $aFED01000932711 035 $a(Aleph)000932711FED01 035 $a000932711 100 $a20110307d2010----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $ay-------001yy 200 1 $aAnatomia delle Brigate rosse$ele radici ideologiche del terrorismo rivoluzionario$fAlessandro Orsini 205 $a2. ed. 210 $aSoveria Mannelli$cRubbettino$d2010 215 $aX, 466 p.$d23 cm 225 1 $aSaggi$v254 610 0 $aBrigate rosse 676 $a322.420$v21$zita 700 1$aOrsini,$bAlessandro$f<1975- >$0328972 801 0$aIT$bUNINA$gREICAT$2UNIMARC 901 $aBK 912 $a990009327110403321 952 $aCollez. 2075 (254)$b46343$fFSPBC 959 $aFSPBC 996 $aAnatomia delle Brigate rosse$9766055 997 $aUNINA LEADER 01921nam 2200505I 450 001 9910704910903321 005 20140908093724.0 035 $a(CKB)5470000002446640 035 $a(OCoLC)890130997 035 $a(EXLCZ)995470000002446640 100 $a20140908j201301 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 14$aThe influence of unsteadiness on the analysis of pressure gain combustion devices /$fDaniel E. Paxson, Tom Kaemming 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJanuary 2013. 215 $a1 online resource (16 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2013-217831 300 $aTitle from title screen (viewed July 9, 2014). 300 $a"January 2013." 300 $a"Prepared for the 51st Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics, Grapevine, Texas, January 7-10, 2013." 300 $a"AIAA-2013-0280." 320 $aIncludes bibliographical references (page 16). 606 $aThermodynamic efficiency$2nasat 606 $aCombustion$2nasat 606 $aPerformance prediction$2nasat 606 $aThermodynamic cycles$2nasat 606 $aSteady flow$2nasat 615 7$aThermodynamic efficiency. 615 7$aCombustion. 615 7$aPerformance prediction. 615 7$aThermodynamic cycles. 615 7$aSteady flow. 700 $aPaxson$b Daniel E.$01386438 702 $aKaemming$b Tom 712 02$aNASA Glenn Research Center, 712 02$aUnited States.$bNational Aeronautics and Space Administration, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910704910903321 996 $aThe influence of unsteadiness on the analysis of pressure gain combustion devices$93439579 997 $aUNINA LEADER 01667nam 22005773 450 001 9910156329203321 005 20250102080301.0 010 $a9783318034264 010 $a3318034266 035 $a(CKB)3780000000101137 035 $a(MiAaPQ)EBC31866746 035 $a(Au-PeEL)EBL31866746 035 $a(OCoLC)1046109982 035 $a(SZ-BaSKA)222319 035 $a(EXLCZ)993780000000101137 100 $a20250102d1992 uy 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAntibodies As Carriers of Cytotoxicity 205 $a1st ed. 210 1$aBasel :$cS. Karger AG,$d1992. 210 4$dİ1992. 215 $a1 online resource (221 pages) 225 1 $aIssn Series 311 08$a9783805555999 311 08$a3805555997 410 0$aIssn Series 606 $aAntibody-toxin conjugates$xTherapeutic use$xTesting 606 $aCancer$xChemotherapy$xEvaluation 615 0$aAntibody-toxin conjugates$xTherapeutic use$xTesting. 615 0$aCancer$xChemotherapy$xEvaluation. 676 $a616.07/93 700 $aSedlacek$b H. H$0863253 701 $aSeemann$b G$01781548 701 $aHoffmann$b D$01781549 701 $aCzech$b J$0335485 701 $aLorenz$b P$01781550 701 $aKolar$b C$01781551 701 $aBosslet$b K$01781552 701 $aQueisser$b W$01215483 701 $aScheithauer$b W$01781553 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910156329203321 996 $aAntibodies As Carriers of Cytotoxicity$94306405 997 $aUNINA