Recent advances in correlation and integration between vibration control, energy harvesting and monitoring
Traditional structures adopt a split design with vibration control, energy harvesting and
monitoring, which is difficult to meet the needs of technological development. The …
monitoring, which is difficult to meet the needs of technological development. The …
Experimental and numerical nonlinear stability analysis of wings incorporating flared folding wingtips
Recent studies have considered the use of wings incorporating flared folding wingtips
(FFWTs) to enable higher aspect ratios (reducing overall induced drag) while also reducing …
(FFWTs) to enable higher aspect ratios (reducing overall induced drag) while also reducing …
On the dynamic behavior of wings incorporating floating wingtip fuel tanks
Recent studies have shown that semi-aeroelastic hinge devices can enable larger aircraft
wingspans. Such a device would be folded on the ground to meet airport width restrictions …
wingspans. Such a device would be folded on the ground to meet airport width restrictions …
Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge
There has been a growing interest in utilizing flared folding wingtips as an in-flight load
alleviation device to enable increased wing spans that meet airport gate limits but with little …
alleviation device to enable increased wing spans that meet airport gate limits but with little …
Nonlinear Multibody Modelling of Flexible Aircraft with Flared Hinged Wings
CW Cheng, A Cea, R Palacios, A Castrichini… - AIAA Scitech 2024 …, 2024 - arc.aiaa.org
This paper presents a comprehensive study on the modelling, verification, and dynamic
analysis of a flexible multibody flared hinged wing system. A geometrically-exact composite …
analysis of a flexible multibody flared hinged wing system. A geometrically-exact composite …
[PDF][PDF] Gust load alleviation wind tunnel tests of a folding wing tip configuration
Increasing the aspect ratio is one way to improve aircraft aerodynamic efficiency. This
reduces the induced drag term but, at the same time, produces an increment of the wing …
reduces the induced drag term but, at the same time, produces an increment of the wing …
Nonlinear Aeroelastic Response Analysis of Wing with Flared Folding Wingtip
J Han, Z Wu, C Yang - Journal of Aerospace Engineering, 2024 - ascelibrary.org
The use of flared folding wingtip (FFWT) for load alleviation has been considered in recent
studies. Most studies analyzed FFWT based on the linear assumption and ignored the …
studies. Most studies analyzed FFWT based on the linear assumption and ignored the …
Nonlinear Stability Analysis of Floating Wingtips with Control Surface Freeplay
Flared folding wingtip (FFWT) devices have been shown to enable higher aspect ratios in
future aircraft designs while meeting airport width restrictions and reducing the loads …
future aircraft designs while meeting airport width restrictions and reducing the loads …
Experimental Effect of Sideslip Angle on the Dynamic Behaviour of Flared Folding Wingtips
View Video Presentation: https://doi. org/10.2514/6.2023-0376. vid A concept of growing
interest in recent years is the Flared Folding Wingtip (FFWT), which can be used in-flight to …
interest in recent years is the Flared Folding Wingtip (FFWT), which can be used in-flight to …
[PDF][PDF] CONSTRAINED FLEXIBLE WING WITH FOLDING WINGTIP DYNAMICS MODEL BASED ON LAGRANGE'S METHOD
L Dehmlow, PJ González, G Stavorinus, FJ Silvestre - conf.ifasd2024.nl
CONSTRAINED FLEXIBLE WING WITH FOLDING WINGTIP DYNAMICS MODEL BASED ON
LAGRANGE’S METHOD Page 1 International Forum on Aeroelasticity and Structural Dynamics …
LAGRANGE’S METHOD Page 1 International Forum on Aeroelasticity and Structural Dynamics …