1989
DOI: 10.1016/0022-460x(89)91005-5
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On coupled bending and torsional vibration of uniform beams

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Cited by 122 publications
(51 citation statements)
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“…The free vibration analysis of such beams has been addressed in the literature [2}4]. In the relatively simpler case when the cross-section of the beam has a single axis of symmetry, the free vibratory modes consist of bending displacements in one plane which are coupled with torsional rotation, and the bending displacements in the other plane which are de-coupled from torsion [5,6]. A high aspect ratio aircraft wing can be idealized as a bending}torsion coupled beam [7,8] for which the torsional coupling occurs only in one of the principal planes of bending.…”
Section: Theorymentioning
confidence: 99%
“…The free vibration analysis of such beams has been addressed in the literature [2}4]. In the relatively simpler case when the cross-section of the beam has a single axis of symmetry, the free vibratory modes consist of bending displacements in one plane which are coupled with torsional rotation, and the bending displacements in the other plane which are de-coupled from torsion [5,6]. A high aspect ratio aircraft wing can be idealized as a bending}torsion coupled beam [7,8] for which the torsional coupling occurs only in one of the principal planes of bending.…”
Section: Theorymentioning
confidence: 99%
“…Since, for a physical problem, the coefficients a, b, c and d are always positive reals, being c less than one, it is possible to show, [10] that all eight roots of the polynomial (19) are…”
Section: Analytical Solutionmentioning
confidence: 99%
“…Equations for the equilibrium in terms of components for an orthotropic thin circular cylindrical shell subjected to a load that is symmetric about the shell result in an eighth-order differential equations as shown by Paliwal and Pande [7]. Bishop et al [8] showed that an eighth-order differential equation arises in torsional vibration of uniform beams. Existence and uniqueness of solutions of 2n-th order boundary value problems are discussed by Agarwal [9,10].…”
Section: Introductionmentioning
confidence: 99%