Complex nonlinear dynamics and vibration suppression of conceptual airfoil models: A state-of-the-art overview

Q Liu, Y Xu, J Kurths, X Liu - Chaos: An Interdisciplinary Journal of …, 2022 - pubs.aip.org
During the past few decades, several significant progresses have been made in exploring
complex nonlinear dynamics and vibration suppression of conceptual aeroelastic airfoil …

[HTML][HTML] Experimental and numerical investigation of an aircraft wing with hinged wingtip for gust load alleviation

D Balatti, HH Khodaparast, MI Friswell… - Journal of Fluids and …, 2023 - Elsevier
A recent consideration in aircraft design is using hinged wing tip devices to increase the
aspect ratio, improving aircraft performance. Moreover, numerical studies have suggested …

Probabilistic regularization load reconstruction method based on iterative strategy

B Lin, Q Shi, C Yang, K Hu, F Zhu - Journal of Sound and Vibration, 2025 - Elsevier
In view of the poor solution accuracy of the traditional Green's function-based load
reconstruction method, this paper proposes a load reconstruction method based on an …

Vibration energy harvesting by means of piezoelectric patches: application to aircrafts

D Tommasino, F Moro, B Bernay… - Sensors, 2022 - mdpi.com
Vibration energy harvesters in industrial applications usually take the form of cantilever
oscillators covered by a layer of piezoelectric material and exploit the resonance …

[HTML][HTML] Experimental and numerical gust identification using deep learning models

K Lakshmanan, D Balatti, HH Khodaparast… - Applied Mathematical …, 2024 - Elsevier
Identifying gusts and turbulence events is of primary importance for designing future gust
load alleviation systems, calculating airframe load, and analysing incidents. Due to the …

Improving wind tunnel “1-cos” gust profiles

D Balatti, H Haddad Khodaparast, MI Friswell… - Journal of Aircraft, 2022 - arc.aiaa.org
A vane-type gust generator has been designed and characterized in the Swansea University
wind tunnel to enable the validation of the response of aircraft models to gust loads. The …

Active disturbance rejection controller design for alleviation of gust-induced aeroelastic responses

C Yue, Y Zhao - Aerospace Science and Technology, 2023 - Elsevier
This paper develops an active disturbance rejection control technology that uses the
equivalent input disturbance (EID) approach to reduce the aeroelastic vibrations and …

Inverse analysis of radiative properties of internal medium and surface for cylindrical system using CSM-CGM approach

C Zhang, BW Li, RR Zhou, PX Li, LY Huang - International Journal of …, 2023 - Elsevier
An inverse analysis is conducted to simultaneously estimate the radiative properties in a 2D
cylindrical system including the extinction coefficient, scattering albedo, and the wall …

Active hinged wingtip for gust load alleviation and manoeuvres

D Balatti, JD Ellis, S JiffrI… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-2567. vid The development of
lighter and more efficient transport aircraft has led to an increased focus on gust load …

Effects of structural geometric nonlinearities on the transonic aeroelastic characteristics of wing

K Ye, M Yang, L Qin, R Xue, Z Ye - Aerospace Science and Technology, 2024 - Elsevier
The structural geometric nonlinearity has a great influence on the transonic aeroelastic
characteristics of aircraft wings, which is an important problem for the aerodynamic and …