2019
DOI: 10.1016/j.compstruct.2018.10.035
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Aeroelastic stability analysis of curved composite panels with embedded Macro Fiber Composite actuators

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Cited by 30 publications
(8 citation statements)
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“…According to the stress-strain relationship, Equations (11) and (19) are translated into the system of strain partial differential equations of the upper surface of the MFC and the upper surface of the plate:…”
Section: The Actuating Equation Of An Mfc Laminated Plate Structurementioning
confidence: 99%
See 2 more Smart Citations
“…According to the stress-strain relationship, Equations (11) and (19) are translated into the system of strain partial differential equations of the upper surface of the MFC and the upper surface of the plate:…”
Section: The Actuating Equation Of An Mfc Laminated Plate Structurementioning
confidence: 99%
“…Equations (9), (11) and (31) are combined to obtain the interfacial shear stress between the MFC and the plate structure along the direction of the x axis, namely, the actuating stress of the MFC along the direction of the x axis:…”
Section: The Actuating Equation Of An Mfc Laminated Plate Structurementioning
confidence: 99%
See 1 more Smart Citation
“…In addition, Gawryluk et al [12] analyzed the problem of vibration reduction in a cantilever beam with an embedded MFC actuator under kinematic excitation. Zhou et al [13] investigated the aeroelastic stability of curved composite panels with embedded MFC actuators in a supersonic airflow.…”
Section: Introductionmentioning
confidence: 99%
“…Static, buckling and dynamic analyses of laminated composite plates with MFC actuators have been extensively investigated [8][9][10][11][12][13][50][51][52][53][54]. In addition, piezoelectric materials were used in the smart structures for shape, vibration and buckling control [7,12,[55][56][57].…”
Section: Introductionmentioning
confidence: 99%