Results 51 to 60 of about 7,826 (224)

Investigation of a Morphing Wing Capable of Airfoil and Span Adjustment Using a Retractable Folding Mechanism

open access: yesAerospace, 2019
The presented aircraft is capable of alternating between two singular working points by folding the exterior surfaces of the wing underneath the interior surfaces. This allows for a significant change in wingspan, lift surfaces, aspect ratio and airfoil (
Amit Geva, Haim Abramovich, Rimon Arieli
doaj   +1 more source

Perspectives on Highly Adaptive or Morphing Aircraft [PDF]

open access: yes, 2009
The ability to adapt to different flight conditions has been fundamental to aircraft design since the Wright Brothers first flight. Over a hundred years later, unconventional aircraft adaptability, often called aircraft morphing has become a topic of ...
Busan, Ronald C.   +3 more
core   +1 more source

Evaluation of a Compliant Droop-Nose Morphing Wing Tip via Experimental Tests [PDF]

open access: yes, 2017
A morphing droop-nose wing tip with span of 1.3 m and target 2 deg droop was designed, manufactured, and tested as part of the European project Novel Air Vehicle Configurations: From Fluttering Wings to Morphing Flight.
Cheung, Ronald   +6 more
core   +2 more sources

Active Metamaterials with Tunable Shear Nonreciprocity and Nonlinear Dynamics

open access: yesAdvanced Science, EarlyView.
Active gear‐based mechanical metamaterials enable simultaneous control of translational and torsional stiffnesses by 30–100×, break shear reciprocity under positive versus negative loads, broadly tune resonant frequencies, and offer programmable dynamic responses.
Xin Fang, Miao Yu, Dianlong Yu, Li Cheng
wiley   +1 more source

Rigid–Elastic Coupling Dynamics of Morphing Wing Aircraft

open access: yesAerospace
This paper presents a rigid–elastic coupling dynamic model for a morphing aircraft with variable-sweep wings, developed using Kane’s method. The model accurately captures the interactions between flight dynamics and structural dynamics during morphing ...
Siyu Hua, Xugang Wang, Zhongyuan Wang
doaj   +1 more source

Coupled Transport/Hyperelastic Model for High Energy Density Nastic Materials [PDF]

open access: yes, 2006
A new development in aerospace technology involves the creation of aircraft that can undergo large changes in the shape of their wings and control surfaces.
Homison, Christopher Joseph
core  

Roadmap on Artificial Intelligence‐Augmented Additive Manufacturing

open access: yesAdvanced Intelligent Systems, EarlyView.
This Roadmap outlines the transformative role of artificial intelligence‐augmented additive manufacturing, highlighting advances in design, monitoring, and product development. By integrating tools such as generative design, computer vision, digital twins, and closed‐loop control, it presents pathways toward smart, scalable, and autonomous additive ...
Ali Zolfagharian   +37 more
wiley   +1 more source

Design of a Variable-Stiffness Compliant Skin for a Morphing Leading Edge

open access: yesApplied Sciences, 2021
A seamless and smooth morphing leading edge has remarkable potential for noise abatement and drag reduction of civil aircraft. Variable-stiffness compliant skin based on tailored composite laminate is a concept with great potential for morphing leading ...
Zhigang Wang, Yu Yang
doaj   +1 more source

Onboard Trajectory Generation of Hypersonic Morphing Aircraft

open access: yesInternational Journal of Aerospace Engineering, 2021
In this paper, a trajectory optimization strategy for the hypersonic morphing aircraft is proposed, and the AMPI method is used to generate the online trajectory with initial state errors. Firstly, the aerodynamic model and propulsion model of the hypersonic morphing aircraft were established considering the wingspan and the scramjet.
Chenxin Zhang   +2 more
openaire   +2 more sources

Snap-through behaviour of a bistable structure based on viscoelastically generated prestress [PDF]

open access: yes, 2017
A novel form of shape-changing bistable structure has been successfully developed through the use of viscoelastically generated prestress. Bistability is achieved through pairs of deflecting viscoelastically prestressed polymeric matrix composite (VPPMC)
Fancey, Kevin S., Ge, Chao, Wang, Bing
core   +1 more source

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