Recent developments in the aeroelasticity of morphing aircraft
RM Ajaj, MS Parancheerivilakkathil… - Progress in Aerospace …, 2021 - Elsevier
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 …
A review on evolution of aeroelastic assisted wing
P Sivanandi, C Gupta, H Durai - International Journal of Aeronautical and …, 2023 - Springer
Aeroelastic wings have a significant capacity like normal flyers, to improve the aircraft's
overall performance and maneuverability. It is a plugin that allows changing the airfoil-level …
overall performance and maneuverability. It is a plugin that allows changing the airfoil-level …
Folding wingtips for improved roll performance
F Healy, R Cheung, T Neofet, M Lowenberg… - Journal of Aircraft, 2022 - arc.aiaa.org
Future aircraft designs look set to use longer wingspans to increase the aspect ratio and
therefore overall aerodynamic efficiency of the airframe. Such larger wingspans also reduce …
therefore overall aerodynamic efficiency of the airframe. Such larger wingspans also reduce …
[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 …
Sizing of high-aspect-ratio wings with folding wingtips
High-aspect-ratio wings are of particular interest to modern aircraft design due to the
inherent reduction in induced drag that they provide. However, such wing configurations …
inherent reduction in induced drag that they provide. However, such wing configurations …
Passive gust alleviation of a flying-wing aircraft by analysis and wind-tunnel test of a scaled model in dynamic similarity
S He, S Guo, Y Liu, W Luo - Aerospace Science and Technology, 2021 - Elsevier
An investigation was conducted to evaluate the effectiveness of a passive gust alleviation
device (PGAD) installed in a flying-wing aircraft of 62.3 m wing span at large swept back …
device (PGAD) installed in a flying-wing aircraft of 62.3 m wing span at large swept back …
Strain-based geometrically nonlinear beam formulation for rigid–flexible multibody dynamic analysis
Geometrically nonlinear strain-based beam formulation has the potential to analyze flexible
slender components in multibody systems efficiently owing to the minimum number of …
slender components in multibody systems efficiently owing to the minimum number of …
Unsteady aeroelastic analysis of the semi aeroelastic hinge including local geometric nonlinearities
P Mastracci, F Saltari, F Mastroddi, T Wilson… - AIAA Journal, 2022 - arc.aiaa.org
A recent consideration in aircraft design is the use of folding wing tips, with the aim of
enabling higher aspect ratio wings with less induced drag but also meeting airport gate …
enabling higher aspect ratio wings with less induced drag but also meeting airport gate …
Actuated adaptive wingtips on transport aircraft: Requirements and preliminary design using pressure-actuated cellular structures
Folding wingtip technologies are in the focus of research for their potential to significantly
reduce the induced drag of transport aircraft by increasing the wing's aspect ratio in flight …
reduce the induced drag of transport aircraft by increasing the wing's aspect ratio in flight …
Quasi-steady aeroelastic analysis of the semi-aeroelastic hinge including geometric nonlinearities
A recent consideration in aircraft design is the use of folding wingtips, with the aim of
enabling higher-aspect-ratio wings with less induced drag but also meeting airport gate …
enabling higher-aspect-ratio wings with less induced drag but also meeting airport gate …