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001 9910705667303321
005 20170908135815.0
035   $a(CKB)5470000002451722
035   $a(OCoLC)986530696
035   $a(EXLCZ)995470000002451722
100   $a20170510j200208    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTransient vibration prediction for rotors on ball bearings using load-dependent non-linear bearing stiffness /$fDavid P. Fleming, J.V. Poplawski
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dOctober 2002.
215   $a1 online resource (7 pages) $cillustrations
225 1 $aNASA/TM ;$v2002-211829
300   $a"August 2002."
300   $a"Prepared for the IFToMM Sixth International Conference on Rotor Dynamics sponsored by the National Committee of Applied Mechanics of The Institution of Engineers, Sydney, Australia, September 30-October 3, 2002."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
320   $aIncludes bibliographical references (page 7).
606   $aRotor dynamics$2nasat
606   $aBall bearings$2nasat
606   $aRoller bearings$2nasat
606   $aStiffness$2nasat
606   $aLoads (forces)$2nasat
615  7$aRotor dynamics.
615  7$aBall bearings.
615  7$aRoller bearings.
615  7$aStiffness.
615  7$aLoads (forces)
700   $aFleming$b David P.$01398755
702   $aPoplawski$b J. V$g(Joseph V.),
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910705667303321
996   $aTransient vibration prediction for rotors on ball bearings using load-dependent non-linear bearing stiffness$93493920
997   $aUNINA