2020
DOI: 10.1016/j.jfluidstructs.2020.102986
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Limit cycle characterization of an aeroelastic wing in a bluff body wake

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Cited by 10 publications
(1 citation statement)
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“…It should be noted that due to the complexity of the solution, there are fewer and fewer analytical studies on the dynamics, stability and flutter of aircraft components, including wing airfoils. Among the latter, we note [Al-Mashhadani et al, 2017;Balakrishnan et al, 2014;Shubov, 2014;Yonghong Li and Ning Qin, 2021;Zachary et al, 2020]. In contrast to the direct Lyapunov method used in this work, the presented works use frequency methods suitable only for studying linear systems, various numerical methods, experimental studies.…”
Section: Introductionmentioning
confidence: 99%
“…It should be noted that due to the complexity of the solution, there are fewer and fewer analytical studies on the dynamics, stability and flutter of aircraft components, including wing airfoils. Among the latter, we note [Al-Mashhadani et al, 2017;Balakrishnan et al, 2014;Shubov, 2014;Yonghong Li and Ning Qin, 2021;Zachary et al, 2020]. In contrast to the direct Lyapunov method used in this work, the presented works use frequency methods suitable only for studying linear systems, various numerical methods, experimental studies.…”
Section: Introductionmentioning
confidence: 99%