LEADER 00864nam0-2200325---450- 001 990009844640403321 005 20140401134800.0 010 $a978-88-15-24158-0 035 $a000984464 035 $aFED01000984464 035 $a(Aleph)000984464FED01 035 $a000984464 100 $a20140401d2012----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $aa-------001yy 200 1 $aAustralia$fCarla Bassu 210 $aBologna$cil Mulino$d2012 215 $a155 p.$cill.$d21 cm 225 1 $aSi governano cosė$v18 610 0 $aAustralia$aOrdinamento istituzionale 676 $a342.94$v22$zita 700 1$aBassu,$bCarla$0479535 801 0$aIT$bUNINA$gREICAT$2UNIMARC 901 $aBK 912 $a990009844640403321 952 $aCollez. 2108 (18)$b51491$fFSPBC 959 $aFSPBC 996 $aAustralia$9826278 997 $aUNINA LEADER 01915nam 2200517I 450 001 9910705297303321 005 20140320153822.0 035 $a(CKB)5470000002448389 035 $a(OCoLC)873950466 035 $a(EXLCZ)995470000002448389 100 $a20140319d1983 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 14$aThe influence of gyroscopic forces on the dynamic behavior and flutter of rotating blades /$fF. Sisto and A.T. Chang 210 1$aHoboken, N.J. :$cDepartment of Mechanical Engineering, Stevens Institute of Technology ;$aCleveland, Ohio :$cLewis Research Center, National Aeronautics and Space Administration,$d1983. 215 $a1 online resource (95 pages, 19 unnumbered pages) $cillustrations 225 1 $aNASA-CR ;$v175444 300 $aTitle from title screen (viewed on Mar. 19, 2014). 300 $a"December 1983." 300 $a"Report no. ME-RT-82006." 320 $aIncludes bibliographical references (pages 94-95). 606 $aCantilever members$2nasat 606 $aDynamic structural analysis$2nasat 606 $aFinite element method$2nasat 606 $aForced vibration$2nasat 606 $aPrecession$2nasat 606 $aTurbomachine blades$2nasat 615 7$aCantilever members. 615 7$aDynamic structural analysis. 615 7$aFinite element method. 615 7$aForced vibration. 615 7$aPrecession. 615 7$aTurbomachine blades. 700 $aSisto$b Fernando$01401958 702 $aChang$b A. T. 712 02$aStevens Institute of Technology, 712 02$aLewis Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910705297303321 996 $aThe influence of gyroscopic forces on the dynamic behavior and flutter of rotating blades$93471452 997 $aUNINA