Linear vibrations are studied for a straight uniform finite beam element of general orientation spinning at a constant angular speed about a fixed axis in the inertial space. The gyroscopic and circulatory matrices and also the geometric stiffness matrix of the beam element are presented. The effect of the centrifugal static axial load on the bending and torsional dynamic stiffnesses is thereby accounted for. The Rayleigh/Timoshenko/Saint-Venant theory is applied, and polynomial shape functions are used in the construction of the deformation fields. Nonzero off-diagonal elements in the gyroscopic and circulatory matrices indicate coupled bending/shearing/torsional/tensional free and forced modes of a generally oriented spinning beam. Two numerical examples demonstrate the use and performance of the beam element.
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January 1996
Research Papers
A Spinning Finite Beam Element of General Orientation Analyzed With Rayleigh/Timoshenko/Saint-Venant Theory
T. J. S. Abrahamsson,
T. J. S. Abrahamsson
Saab Military Aircraft, Linko¨ping, Sweden
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J. H. Sa¨llstro¨m
J. H. Sa¨llstro¨m
Division of Solid Mechanics, Chalmers University of Technology, Go¨teborg, Sweden
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T. J. S. Abrahamsson
Saab Military Aircraft, Linko¨ping, Sweden
J. H. Sa¨llstro¨m
Division of Solid Mechanics, Chalmers University of Technology, Go¨teborg, Sweden
J. Eng. Gas Turbines Power. Jan 1996, 118(1): 86-94 (9 pages)
Published Online: January 1, 1996
Article history
Received:
February 4, 1994
Online:
November 19, 2007
Citation
Abrahamsson, T. J. S., and Sa¨llstro¨m, J. H. (January 1, 1996). "A Spinning Finite Beam Element of General Orientation Analyzed With Rayleigh/Timoshenko/Saint-Venant Theory." ASME. J. Eng. Gas Turbines Power. January 1996; 118(1): 86–94. https://doi.org/10.1115/1.2816554
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