Recent advances in experimental and numerical methods for dynamic analysis of floating offshore wind turbines—An integrated review

A Subbulakshmi, M Verma, M Keerthana… - … and Sustainable Energy …, 2022 - Elsevier
Over the past decade, there has been rapid increase in the offshore wind turbine
installations. The future installations will see a progression from shallow to deep waters. It …

Progress of combined wind and wave energy harvesting devices and related coupling simulation techniques

F Cao, M Yu, B Liu, Z Wei, L Xue, M Han… - Journal of Marine Science …, 2023 - mdpi.com
The use of combined wind and wave energy harvesting devices (CWWHDs) is an effective
way to synergistically capture offshore wind and wave energy. However, the form of …

[HTML][HTML] Computational aeroelastic analysis of wings based on the structural discontinuous Galerkin and aerodynamic vortex lattice methods

V Gulizzi, I Benedetti - Aerospace Science and Technology, 2024 - Elsevier
An original computational framework for the aeroelastic analysis of wings featuring general
transverse section is developed. The framework is based on the coupling between a novel …

Adjoint-free aerodynamic shape optimization of the common research model wing

J Li, M Zhang - AIAA Journal, 2021 - arc.aiaa.org
Adjoint-free methods are required in aerodynamic shape design optimization if an adjoint
solver is unavailable. However, their performance is highly criticized in high-dimensional …

Morphing wing, UAV and aircraft multidisciplinary studies at the Laboratory of Applied Research in Active Controls, Avionics and AeroServoElasticity LARCASE

RM Botez - Aerospace Lab, 2018 - hal.science
Several large-scale projects were carried out at the LARCASE at ÉTS in numerical studies
and experimental tests for morphing aircraft using three equipments. In this article, these …

Review of vortex lattice method for supersonic aircraft design

H Joshi, P Thomas - The Aeronautical Journal, 2023 - cambridge.org
There has been a renewed interest in develo** environmentally friendly, economically
viable, and technologically feasible supersonic transport aircraft and reduced order …

[HTML][HTML] Seamless morphing trailing edge flaps for UAS-S45 using high-fidelity aerodynamic optimization

MH Negahban, M Bashir, V Traisnel… - Chinese Journal of …, 2024 - Elsevier
The seamless trailing edge morphing flap is investigated using a high-fidelity steady-state
aerodynamic shape optimization to determine its optimum configuration for different flight …

Enhanced range and endurance evaluation of a camber morphing wing aircraft

BW Jo, T Majid - Biomimetics, 2023 - mdpi.com
Flight range, endurance, maneuverability, and agility are the key elements that determine an
aircraft's performance. Both conventional and morphing wing aircraft have been well studied …

Effects of an unsteady morphing wing with seamless side-edge transition on aerodynamic performance

C Abdessemed, A Bouferrouk, Y Yao - Energies, 2022 - mdpi.com
This paper presents an unsteady flow analysis of a 3D wing with a morphing trailing edge
flap (TEF) and a seamless side-edge transition between the morphed and static parts of a …

[HTML][HTML] A study of morphing aircraft on morphing rules along trajectory

C **aoyu, LI Chunna, G Chunlin, GU Liangxian… - Chinese Journal of …, 2021 - Elsevier
Morphing aircraft can meet requirements of multi-mission during the whole flight due to
changing the aerodynamic shape, so it is necessary to study its morphing rules along the …