01958oam 2200541 450 991070745480332120160819163412.0(CKB)5470000002464980(OCoLC)762106559(EXLCZ)99547000000246498020111122j198012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierVibration characteristics of a steadily rotating slender ring /Frederick J. Lallman[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,December 1980.1 online resource (97 pages) illustrationsNASA technical paper ;1775Title from title screen (viewed on Aug. 18, 2016)."December 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 61).Dynamic structural analysisnasatMoments of inertianasatPartial differential equationsnasatSpacecraft designnasatVibration modenasatDynamic structural analysis.Moments of inertia.Partial differential equations.Spacecraft design.Vibration mode.Lallman Frederick J.1403029Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOGPOBOOK9910707454803321Vibration characteristics of a steadily rotating slender ring3474757UNINA