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200 10$aVibration characteristics of a steadily rotating slender ring /$fFrederick J. Lallman
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dDecember 1980.
215   $a1 online resource (97 pages) $cillustrations
225 1 $aNASA technical paper ;$v1775
300   $aTitle from title screen (viewed on Aug. 18, 2016).
300   $a"December 1980."
300   $a"Performing Organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 61).
606   $aDynamic structural analysis$2nasat
606   $aMoments of inertia$2nasat
606   $aPartial differential equations$2nasat
606   $aSpacecraft design$2nasat
606   $aVibration mode$2nasat
615  7$aDynamic structural analysis.
615  7$aMoments of inertia.
615  7$aPartial differential equations.
615  7$aSpacecraft design.
615  7$aVibration mode.
700   $aLallman$b Frederick J.$01403029
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
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996   $aVibration characteristics of a steadily rotating slender ring$93474757
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