1992
DOI: 10.1016/0045-7949(92)90189-7
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Frequencies of rotating tapered timoshenko beams with different boundary conditions

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Cited by 31 publications
(23 citation statements)
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“…Centrifugal force K Flexural stiffness matrix K G Geometric stiffness matrix K II , K JJ Nodal stiffness matrices of nodes (1) and (2) Rotating beams are widely used in the aerospace and mechanical engineering structures such as helicopter rotor blades, spacecraft with flexible appendages and windmills; thus, they have been extensively studied [1][2][3][4][5][6][7]. Understanding the response of these elements to both static and dynamic loads provides designers with important information to evaluate the performance of rotating machinery.…”
Section: A(x)mentioning
confidence: 99%
“…Centrifugal force K Flexural stiffness matrix K G Geometric stiffness matrix K II , K JJ Nodal stiffness matrices of nodes (1) and (2) Rotating beams are widely used in the aerospace and mechanical engineering structures such as helicopter rotor blades, spacecraft with flexible appendages and windmills; thus, they have been extensively studied [1][2][3][4][5][6][7]. Understanding the response of these elements to both static and dynamic loads provides designers with important information to evaluate the performance of rotating machinery.…”
Section: A(x)mentioning
confidence: 99%
“…(19)(20)(21)(22)(23)(24)(25)(26)(27) at x 0 = 0, and using the correlations defined in Table 2, the following equations are obtained Table 3 DTM theorems adopted for boundary conditions…”
Section: Solutionmentioning
confidence: 99%
“…Yokoyama [26] used the finite element method to calculate the natural frequency of rotating uniform Timoshenko beams. Khulief and Bazoune [27] developed finite element method for different deformation, rotary inertia and centrifugal stiffening and solved rotating tapered Timoshenko beams for different combinations of the fixed, hinged and free boundary conditions. The free vibration characteristics of rotating Timoshenko beams have been subject to extensive studies by Lee and Lin [28], Du et al [29], Nagaraj [30] and Lin and Hsiao [31].…”
mentioning
confidence: 99%
“…Bazoune and Khulief [3] developed a finite beam element for vibration analysis of a rotating double-tapered Timoshenko beam. Khulief and Bazoune [9] extended the work in Bazoune and Khulief [3] to account for different combinations of the fixed, hinged, and free end conditions. In this study, as an extension of the authors' previous works [8,17,18], free vibration analysis of a rotating, double-tapered, cantilever Timoshenko beam that undergoes flapwise bending vibration is performed using the differential transform method (DTM), which is an iterative procedure to obtain analytic Taylor series solutions of differential equations.…”
Section: Introductionmentioning
confidence: 97%