LEADER 00924nam a2200265 i 4500 001 991001592099707536 005 20020502191503.0 008 970503s1992 it ||| | ita 020 $a8842039470 035 $ab10874975-39ule_inst 035 $aLE02372437$9ExL 040 $aDip.to Studi Storici$bita 082 0 $a909.04924 100 1 $aFoa, Anna$076283 245 10$aEbrei in Europa :$bdalla peste nera all'emancipazione, XIV-XVIII secolo /$cAnna Foa 260 $aRoma ; Bari :$bLaterza,$c1992 300 $aXI, 378 P. 21 cm. 490 0 $aStoria e società 650 4$aEbrei$zEuropa$ySec. 14.-18. 907 $a.b10874975$b23-02-17$c28-06-02 912 $a991001592099707536 945 $aLE023 909.04924 FOA 1 1$g1$i2023000021484$lle023$o-$pE0.00$q-$rl$s- $t0$u1$v0$w1$x0$y.i10983090$z28-06-02 996 $aEbrei in Europa$952362 997 $aUNISALENTO 998 $ale023$b01-01-97$cm$da $e-$fita$git $h0$i1 LEADER 01780nam 2200481 450 001 9910707852803321 005 20161216113557.0 035 $a(CKB)5470000002468030 035 $a(OCoLC)966316292 035 $a(EXLCZ)995470000002468030 100 $a20161216j198405 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAnalysis of lateral and torsional vibration characteristics of beams and shafts with end located rotational masses /$fDaniel K. Robertson 210 1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dMay 1984. 215 $a1 online resource (36 unnumbered pages) $cillustrations 225 1 $aNASA technical memorandum ;$v84593 300 $a"May 1984." 300 $a"Performing organization: NASA Langley Research Center"--Report documentation page. 320 $aIncludes bibliographical references (page [33]). 606 $aAircraft design$2nasat 606 $aBeams (supports)$2nasat 606 $aPartial differential equations$2nasat 606 $aRotation$2nasat 606 $aShafts (machine elements)$2nasat 606 $aVibration$2nasat 615 7$aAircraft design. 615 7$aBeams (supports) 615 7$aPartial differential equations. 615 7$aRotation. 615 7$aShafts (machine elements) 615 7$aVibration. 700 $aRobertson$b Daniel K.$01398874 712 02$aLangley Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910707852803321 996 $aAnalysis of lateral and torsional vibration characteristics of beams and shafts with end located rotational masses$93463101 997 $aUNINA