2019
DOI: 10.1016/j.compstruc.2019.106110
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A partitioned solver to simulate large-displacement fluid–structure interaction of thin plate systems for vibration energy harvesting

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Cited by 14 publications
(2 citation statements)
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“…In other words, current flutter, dominated by bending d mation, is caused by the first-order bending mode. In order to depict the flutter boundary along a Mach number, it is necessary to several simulations for the specified Mach number until the neutral response is achi The practice of identifying critical onset flutter is similar to the studies performe Chawdhury where a detailed flutter analysis is conducted with various wind velo [8,9]. Here, flutter velocity * f V varies through the fixed value of density and manua justment of pressure.…”
Section: Flutter Of Naca 64a010 Airfoilmentioning
confidence: 99%
See 1 more Smart Citation
“…In other words, current flutter, dominated by bending d mation, is caused by the first-order bending mode. In order to depict the flutter boundary along a Mach number, it is necessary to several simulations for the specified Mach number until the neutral response is achi The practice of identifying critical onset flutter is similar to the studies performe Chawdhury where a detailed flutter analysis is conducted with various wind velo [8,9]. Here, flutter velocity * f V varies through the fixed value of density and manua justment of pressure.…”
Section: Flutter Of Naca 64a010 Airfoilmentioning
confidence: 99%
“…Both numerical simulations [1,2] and experimental studies [3,4] have been carried out to study the transonic flutter phenomenon and found that the flutter boundary often shifts with the Mach number. Due to the development of highperformance computing techniques, a variety of efficient effective computational fluid dynamics/computational solid dynamics (CFD/CSD) solvers [5][6][7][8][9] have been developed.…”
Section: Introductionmentioning
confidence: 99%