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    Structure-Actuator Integrated Design of Piezo-Actuated Composite Plate Wing for Active Shape Control 

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 006:;page 04021070-1
    Author(s): Wenya Zhou; Zongyu Zhang; Xiaoming Wang; Weiliang Lv; Xinhan Hu
    Publisher: ASCE
    Abstract: The aerodynamic performance of aircraft can be improved via shape morphing of wings actuated by piezoelectric material. An integrated design approach of piezo-actuated wings was developed while simultaneously considering ...
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    Optimization of Locations and Fiber Orientations of Piezocomposite Actuators on Flexible Wings for Aeroelastic Control 

    Source: Journal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 005
    Author(s): Wenya Zhou; Xiaoming Wang; Wei Qian; Wenhua Wu
    Publisher: American Society of Civil Engineers
    Abstract: Smart piezoelectric fiber composite materials have the potential to improve the aerodynamic properties and aeroelastic responses of flexible wings. Aeroelastic control performance significantly depends on the configurations ...
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    Active Learning Vibration Control of Aero-Engine Blade Based on Kriging Surrogate Optimization Strategy 

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 004:;page 04025045-1
    Author(s): Wenya Zhou; Xinhan Hu; Xiaoming Wang; Jian Xing; Wen Li
    Publisher: American Society of Civil Engineers
    Abstract: In aero-engine failures, a significant proportion is attributed to blade vibration-induced malfunctions. Due to factors such as structural complexity and high stiffness, controlling blade vibration in aero-engines poses a ...
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