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