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Energy harvesting by means of flow-induced vibrations on aerospace vehicles
D Li, Y Wu, A Da Ronch, J **ang - Progress in Aerospace Sciences, 2016 - Elsevier
This paper reviews the design, implementation, and demonstration of energy harvesting
devices that exploit flow-induced vibrations as the main source of energy. Starting with a …
devices that exploit flow-induced vibrations as the main source of energy. Starting with a …
A Smart Wing Model: From Design to Testing in a Wind Tunnel with a Turbulence Generator
The paper concerns the technology of the design, realization, and testing of a flexible smart
wing in a wind tunnel equipped with a turbulence generator. The system of smart wing …
wing in a wind tunnel equipped with a turbulence generator. The system of smart wing …
Suppression of limit cycle oscillations using the nonlinear tuned vibration absorber
The objective of this study is to mitigate, or even completely eliminate, the limit cycle
oscillations in mechanical systems using a passive nonlinear absorber, termed the …
oscillations in mechanical systems using a passive nonlinear absorber, termed the …
Reduced-order modeling for nonlinear aeroelasticity with varying Mach numbers
This paper proposes a nonlinear aerodynamic reduced-order model robust to different Mach
numbers based on a recursive neural network. To model the nonlinear features with varying …
numbers based on a recursive neural network. To model the nonlinear features with varying …
Experimental nonlinear control for flutter suppression in a nonlinear aeroelastic system
Experimental implementation of input–output feedback linearization in controlling the
dynamics of a nonlinear pitch–plunge aeroelastic system is presented. The control objective …
dynamics of a nonlinear pitch–plunge aeroelastic system is presented. The control objective …
Multiple-input multiple-output experimental aeroelastic control using a receptance-based method
This paper presents the first experimental study of multiple-input multiple-output (MIMO)
active vibration suppression by pole placement using the receptance method. The research …
active vibration suppression by pole placement using the receptance method. The research …
[HTML][HTML] Towards nonconservative conditions for equilibrium stability. Applications to switching systems with control delay
The objective of the paper is to give a unitary approach to nonconservative conditions of the
equilibrium stability. The focus is on a real world system defined by a switched linear …
equilibrium stability. The focus is on a real world system defined by a switched linear …
Computational fluid dynamics-based transonic flutter suppression with control delay
Q Zhou, D Li, A Da Ronch, G Chen, Y Li - Journal of Fluids and Structures, 2016 - Elsevier
This work investigates the effects of control input time delay on closed-loop transonic
computational aeroelastic analysis. Control input time delays are becoming critical as the …
computational aeroelastic analysis. Control input time delays are becoming critical as the …
Adaptive feedforward control for gust-induced aeroelastic vibrations
This paper demonstrates the implementation of an adaptive feedforward controller to reduce
structural vibrations on a wing typical section. The aeroelastic model includes a structural …
structural vibrations on a wing typical section. The aeroelastic model includes a structural …
Parametric active aeroelastic control of a morphing wing using the receptance method
H Liu, X Gao, X Wang - Journal of Fluids and Structures, 2020 - Elsevier
This study proposes the parametric active aeroelastic control of a folding wing, which is a
promising concept of morphing wings, by integrating the parameterized aeroservoelastic …
promising concept of morphing wings, by integrating the parameterized aeroservoelastic …