2002
DOI: 10.1006/jsvi.2001.4020
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Transient Analysis of Ring-Stiffened Composite Cylindrical Shells With Both Edges Clamped

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Cited by 25 publications
(7 citation statements)
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“…By substituting (8) in equations (4) and (6), a system of ordinary differential equations in the s-coordinate for the m th circumferential mode can be expressed as follows: with A m is a 10x10 matrix (11)…”
Section: State Vector Of Solutionmentioning
confidence: 99%
See 1 more Smart Citation
“…By substituting (8) in equations (4) and (6), a system of ordinary differential equations in the s-coordinate for the m th circumferential mode can be expressed as follows: with A m is a 10x10 matrix (11)…”
Section: State Vector Of Solutionmentioning
confidence: 99%
“…Recently, the vibration of laminated cylindrical shells with ring stiffeners also has been investigated. Kim and Lee [8] used a theoretical method to examine the effects of ring stiffeners on vibration characteristics and transient responses of the ring-stiffened composite cylindrical shells which subjected to the step pulse loading. The Love's thin shell theory was combined with the discrete stiffener theory to consider the effect of ring stiffeners.…”
Section: Introductionmentioning
confidence: 99%
“…Wang and Lin (2006) studied the dynamic responses of the symmetric cross-ply ring stiffened laminated cylindrical shell by using the modal analysis method. Kim and Lee (2002) employed the Rayleigh-Ritz method and double Fourier series expansion to investigate the transient responses for the ring-stiffened composite cylindrical shells under the step pulse loading. Although the modal analysis method can be effectively used to study the transient responses of the stiffened cylindrical shells, it is difficult to be used to compute the high frequency components which are very important to the early short time transient responses.…”
Section: Introductionmentioning
confidence: 99%
“…Their vibration is solved in Zhang et al [2003]; Xu [2003]; Pellicano and Amabili [2003]. Likewise, in Kim and Lee [2002], , the dynamic behavior of anisotropic and composite shells is solved.…”
Section: Introductionmentioning
confidence: 99%