2017
DOI: 10.1016/j.compstruct.2017.03.007
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Fundamental frequency maximization of orthotropic shells using a free-form optimization method

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Cited by 17 publications
(3 citation statements)
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“…There have been lots of researches to develop effective and efficient design methods to increase the structural fundamental frequency. Shi et al [22] presented a parameter-free approach for a design optimization of orthotropic shells that maximizes fundamental frequencies, where a shape variation was generated by a displacement field due to an external force equivalent to negative shape gradient function. Hu and Tsai [11] found optimal fiber orientation angles to maximize fundamental frequencies of fiber-reinforced laminated cylindrical shells.…”
Section: Introductionmentioning
confidence: 99%
“…There have been lots of researches to develop effective and efficient design methods to increase the structural fundamental frequency. Shi et al [22] presented a parameter-free approach for a design optimization of orthotropic shells that maximizes fundamental frequencies, where a shape variation was generated by a displacement field due to an external force equivalent to negative shape gradient function. Hu and Tsai [11] found optimal fiber orientation angles to maximize fundamental frequencies of fiber-reinforced laminated cylindrical shells.…”
Section: Introductionmentioning
confidence: 99%
“…Aspects of optimization of the composite shells have been studied in Shi et al (2017) and Liu et al (2016). In Shi et al (2017), a free-form optimization method is proposed that maximizes the fundamental frequencies of the orthotropic shells to avoid vibrational resonance.…”
Section: Introductionmentioning
confidence: 99%
“…Aspects of optimization of the composite shells have been studied in Shi et al (2017) and Liu et al (2016). In Shi et al (2017), a free-form optimization method is proposed that maximizes the fundamental frequencies of the orthotropic shells to avoid vibrational resonance. In Liu et al (2016), the structural optimization of a cantilever aircraft wing with stiffeners and curvilinear spars and ribs is described.…”
Section: Introductionmentioning
confidence: 99%