A review of modelling and analysis of morphing wings

D Li, S Zhao, A Da Ronch, J Xiang, J Drofelnik… - Progress in Aerospace …, 2018 - Elsevier
Morphing wings have a large potential to improve the overall aircraft performances, in a way
like natural flyers do. By adapting or optimising dynamically the shape to various flight …

[HTML][HTML] A review of bird-like flapping wing with high aspect ratio

XIE Changchuan, GAO Nongyue, M Yang… - Chinese Journal of …, 2023 - Elsevier
Bird-like flapping-wing vehicles with a high aspect ratio have the potential to fulfill missions
given to micro air vehicles, such as high-altitude reconnaissance, surveillance, rescue, and …

Effect of spanwise folding on the aerodynamic performance of three dimensional flapping flat wing

X Lang, B Song, W Yang, X Yang - Physics of Fluids, 2022 - pubs.aip.org
Bird flight incorporates complex multi-degree-of-freedom motions, such as flapping, pitching,
twisting, and folding. The aerodynamic mechanism of these complex movements, especially …

[HTML][HTML] Delaying stall of morphing wing by periodic trailing-edge deflection

KAN Zi, LI Daochun, J Xiang, C Cheng - Chinese Journal of Aeronautics, 2020 - Elsevier
Morphing wings can improve aircraft performance during different flight phases. Recently
research has focused on steady aerodynamic characteristics of the morphing wing with a …

Code-to-code benchmark for simulation tools based on the unsteady vortex-lattice method

ML Verstraete, LR Ceballos, C Hente… - Journal of Aerospace …, 2023 - arc.aiaa.org
Reliable aerodynamic and aeroelastic simulations of advanced aeronautical/mechanical
systems require us to predict flow-induced forces as accurately as possible. Nowadays …

A co-simulation methodology to simulate the nonlinear aeroelastic behavior of a folding-wing concept in different flight configurations

ML Verstraete, BA Roccia, DT Mook, S Preidikman - Nonlinear Dynamics, 2019 - Springer
A methodology to simulate the unsteady, nonlinear aeroelastic behavior of a folding-wing
concept in multiple flight configurations is presented. It is based on a partitioned or co …

Computational study on aerodynamically coupled piezoelectric harvesters

BA Roccia, ML Verstraete… - Journal of Intelligent …, 2020 - journals.sagepub.com
In this work, the authors present a two-dimensional computational model for predicting the
aeroelastic response as well as the output power of vertically arranged harvesters by taking …

A general numerical unsteady non-linear lifting line model for engineering aerodynamics studies

O Sugar-Gabor - The Aeronautical Journal, 2018 - cambridge.org
The lifting-line theory is widely used for obtaining aerodynamic performance results in
various engineering fields, from aircraft conceptual design to wind-power generation. Many …

[HTML][HTML] Development and application of a mesh generator intended for unsteady vortex-lattice method simulations of wind turbines and wind farms

BA Roccia, LR Ceballos, ML Verstraete… - Wind Energy …, 2024 - wes.copernicus.org
In the last decades, the unsteady vortex-lattice method (UVLM) has gained a lot of
acceptance to study large onshore–offshore wind turbines (WTs). Furthermore, and due to …

Analytical Linearization of Aerodynamic Loads in Unsteady Vortex-Lattice Method for Nonlinear Aeroelastic Applications

C Hente, BA Roccia, R Rolfes, CG Gebhardt - AIAA Journal, 2024 - arc.aiaa.org
This paper presents the analytical linearization of aerodynamic loads (computed with the
unsteady vortex-lattice method), which is formulated as tangent matrices with respect to the …