Recent developments in the aeroelasticity of morphing aircraft
This paper presents an extensive review of the developments in the aeroelasticity of
morphing aircraft that occurred in the last decade (from 2009 to 2020). It focuses mainly on …
morphing aircraft that occurred in the last decade (from 2009 to 2020). It focuses mainly on …
Surrogate-assisted reliability optimisation of an aircraft wing with static and dynamic aeroelastic constraints
This paper presents a numerical strategy for reliability-based design optimisation of an
aircraft wing structure using a surrogate-assisted approach. The design problem is set to …
aircraft wing structure using a surrogate-assisted approach. The design problem is set to …
Aircraft morphing wing design by using partial topology optimization
A morphing wing concept has been investigated over the last decade because it can
effectively enhance aircraft aerodynamic performance over a wider range of flight conditions …
effectively enhance aircraft aerodynamic performance over a wider range of flight conditions …
New conceptual design of aeroelastic wing structures by multi-objective optimization
Internal structural layouts and component sizes of aircraft wing structures have a significant
impact on aircraft performance such as aeroelastic characteristics and mass. This work …
impact on aircraft performance such as aeroelastic characteristics and mass. This work …
Parametric active aeroelastic control of a morphing wing using the receptance method
H Liu, X Gao, X Wang - Journal of Fluids and Structures, 2020 - Elsevier
This study proposes the parametric active aeroelastic control of a folding wing, which is a
promising concept of morphing wings, by integrating the parameterized aeroservoelastic …
promising concept of morphing wings, by integrating the parameterized aeroservoelastic …
Structural and aeroelastic analyses of a wing with tip rotor
X Zhang, M Zhao, H Liang, M Zhu - Journal of Fluids and Structures, 2019 - Elsevier
Based on parametric studies, this paper studies the structural and aerodynamic properties of
a typical wing-rotor system by considering additional coupling effects from the tip rotor. The …
a typical wing-rotor system by considering additional coupling effects from the tip rotor. The …
Reliability-based design optimization of classical wing aeroelasticity
S Sleesongsom, S Yooyen… - IOP Conference …, 2020 - iopscience.iop.org
Flutter speed of aircraft is very important and needs to be firstly specified before a
certification applied for a new aircraft by airworthiness regulator to make sure that the aircraft …
certification applied for a new aircraft by airworthiness regulator to make sure that the aircraft …
Morphing Wing Structural Optimization Using Opposite‐Based Population‐Based Incremental Learning and Multigrid Ground Elements
This paper has twin aims. Firstly, a multigrid design approach for optimization of an
unconventional morphing wing is proposed. The structural design problem is assigned to …
unconventional morphing wing is proposed. The structural design problem is assigned to …
Experimental investigations on structural improvement of morphing mechanism for nose cone of aerospace vehicle adopting a bionic redundant constraint strategy
YL Zhang, CX Li, Y Zhang, QY Cai, SZ Yan - Science China Technological …, 2023 - Springer
Aerospace vehicles have recently received great attention for their completely reusable in
aviation and aerospace. To achieve the optimal aerodynamic performance of the aerospace …
aviation and aerospace. To achieve the optimal aerodynamic performance of the aerospace …
Aircraft morphing systems: Elasticity of selected components and modelling issues
Morphing is an increasingly investigated topic in aeronautics due to the performance
improvements brought by aerodynamic shapes adaptivity on large aircraft. Being …
improvements brought by aerodynamic shapes adaptivity on large aircraft. Being …