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Finite element modeling of a cantilever beamFinite element modeling of uniform cantilever beams and computation of transverse frequencies due to combinations of bending with rotatory inertia and shear flexibility
Document ID
19670013552
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kuzanek, J. F. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1967
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-55743
X-321-67-97
Report Number: NASA-TM-X-55743
Report Number: X-321-67-97
Accession Number
67N22881
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CANTILEVER BEAM
INERTIA
TRANSVERSE VIBRATION
BENDING VIBRATION

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