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Published in 2021 at "Nonlinear Dynamics"
DOI: 10.1007/s11071-021-06577-y
Abstract: The folding wing, as a possible concept for designing morphing aircraft, has gained special attention. However, such a wing may encounter complex nonlinear aeroelastic effects with bilinear-hinge stiffnesses during the in-flight morphing process. This paper… read more here.
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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.03.025
Abstract: Abstract In this paper, an integrated geometrically nonlinear aeroelastic framework to analyze the static nonlinear aeroelastic response of morphing composite wing with orthotropic materials has been developed. A flat plate/shell finite element, which can model… read more here.
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Published in 2021 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2021.106923
Abstract: Abstract Additive manufacturing technology has a potential to improve manufacturing costs and may help to achieve high-performance aerospace structures. One of the application candidates would be a wind tunnel wing model. A wing tunnel model… read more here.
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Published in 2018 at "Engineering Structures"
DOI: 10.1016/j.engstruct.2018.05.073
Abstract: Abstract Aeroelastic structural systems are intrinsically nonlinear and accurate predictions of dynamic responses of nonlinear aeroelastic systems have become of paramount importance since these directly affect the accuracy and reliability of subsequent stability analyses. Such… read more here.
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Published in 2021 at "International Journal of Non-linear Mechanics"
DOI: 10.1016/j.ijnonlinmec.2020.103659
Abstract: Abstract Coupling nonlinear dynamical systems can lead to a host of phenomena, one of which leads to the complete cessation of their oscillations. This phenomenon is referred to as amplitude death (AD) in the dynamical… read more here.
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Published in 2018 at "Journal of Sound and Vibration"
DOI: 10.1016/j.jsv.2018.06.067
Abstract: Abstract This paper studies the effect of shooting and associated local blast induced gust on nonlinear aeroelastic stability and behaviour of a high-aspect ratio wing. The physics of shooting is modeled as a local impulse… read more here.
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Published in 2019 at "Mechanics Based Design of Structures and Machines"
DOI: 10.1080/15397734.2019.1610436
Abstract: Abstract The main aim of this study is to investigate the geometrical nonlinear flutter of three-phase nano-composite plates reinforced with carbon nano-tubes (CNTs). The effective material properties are obtained using Halpin-Tsai relation and rule of… read more here.
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Published in 2021 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/09544100211010963
Abstract: This article presents a fuzzy control method for the limit cycle oscillation (LCO) suppression of nonlinear aeroelastic systems based on the neural network identification algorithm. A prototypical 2D wing section with a single control surface… read more here.
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Published in 2018 at "Journal of Aircraft"
DOI: 10.2514/1.c034684
Abstract: A nonlinear modeling strategy is introduced to drive online optimization-based controllers for trajectory tracking and stabilization of very flexible aircraft. This is achieved thanks to a compact ... read more here.
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Published in 2024 at "AIAA Journal"
DOI: 10.2514/1.j063611
Abstract: The objective of this work is to propose a data-driven Bayesian inference framework to efficiently identify parameters and select models of nonlinear aeroelastic systems. The framework consists of the use of Bayesian theory together with… read more here.
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Published in 2025 at "AIAA Journal"
DOI: 10.2514/1.j064780
Abstract: Nonlinear unsteady aerodynamic reduced-order models (ROMs) based on machine learning or artificial intelligence algorithms can be complex and computationally demanding to train, meaning that for practical aeroelastic applications, the conservative nature of linearization is often… read more here.