2005
DOI: 10.1016/j.jsv.2004.02.046
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A perturbation approach for evaluating natural frequencies of moderately thick elliptic plates

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Cited by 32 publications
(20 citation statements)
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“…= , "° is compared for V 2(1 + ")PP different nodal diameters "m" and nodal circles "n" in Table 2. It can be observed that the results are quite similar, except for the case of m = 1 and n = 1, however, for this case the comparison of the present method with the circular plate, e = 0, seems to be in accordance in contrast with the results obtained by Kaplunov et al [2005], In Table 3, the parameters [3™ m with no nodal diameter m = 0 and one nodal diameter m = 1 are presented. From these results, the frequencies for different values of eccentricity e can be computed.…”
Section: Natural Frequencies Of Almost Circular Plates In Vacuumsupporting
confidence: 69%
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“…= , "° is compared for V 2(1 + ")PP different nodal diameters "m" and nodal circles "n" in Table 2. It can be observed that the results are quite similar, except for the case of m = 1 and n = 1, however, for this case the comparison of the present method with the circular plate, e = 0, seems to be in accordance in contrast with the results obtained by Kaplunov et al [2005], In Table 3, the parameters [3™ m with no nodal diameter m = 0 and one nodal diameter m = 1 are presented. From these results, the frequencies for different values of eccentricity e can be computed.…”
Section: Natural Frequencies Of Almost Circular Plates In Vacuumsupporting
confidence: 69%
“…Next, the natural frequencies for the plate in vacuum are compared with the methods presented in Kaplunov et al [2005].…”
Section: Natural Frequencies Of Almost Circular Plates In Vacuummentioning
confidence: 99%
See 1 more Smart Citation
“…1 and 3. We also mention that the relation (14) has the same form as the dispersion relation for the bending wave on an elastically supported beam, e.g., see Ref. 7.…”
Section: J¼1mentioning
confidence: 89%
“…Instead it provides an equation for the rotation angle θ = ∂W ∂y , evaluated at the edge y = 0, namely, 27) with the constant Q defined in (5.15). The resulting explicit model for the shear edge force is similar to that obtained in respect of a bending moment.…”
Section: (B) Shear Forcementioning
confidence: 99%