Complex nonlinear dynamics and vibration suppression of conceptual airfoil models: A state-of-the-art overview
During the past few decades, several significant progresses have been made in exploring
complex nonlinear dynamics and vibration suppression of conceptual aeroelastic airfoil …
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
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 …
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 …
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 …
oscillators covered by a layer of piezoelectric material and exploit the resonance …
[HTML][HTML] Experimental and numerical gust identification using deep learning models
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 …
load alleviation systems, calculating airframe load, and analysing incidents. Due to the …
Improving wind tunnel “1-cos” gust profiles
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 …
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 …
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 …
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 …
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 …
characteristics of aircraft wings, which is an important problem for the aerodynamic and …