Results 71 to 80 of about 265 (157)
Research on Optimal Morphing Strategies for Multi-Performance of UAV
The flying-wing configuration offers inherent advantages in aerodynamic efficiency and stealth; however, conventional fixed-wing designs face fundamental performance trade-offs when tasked with multi-role missions.
Long Tan, Chao Yang, Yu Wang
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Modern materials and manufacturing technologies have allowed the construction of morphing wings that are able to continuously vary certain airfoil parameters such as twist, camber, or control surface deflection as a function of span. This work presents a
Zachary S. Montgomery +2 more
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Design and Analysis of a Novel Mechanism for the Morphing of Trailing Edge of an Aircraft Wing
In this paper, design of a novel deployable scissor-structural mechanism (SSM) for active camber and chord morphing airfoil has been presented. The mechanism is created via combination of one four-bar linkage and various scissor-like elements (SLEs). The
Şahin Harun Levent, Yaman Yavuz
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Computational Analysis of the Aerodynamics of Camber Morphing
Huntley, Sam +2 more
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The variable camber morphing wing has the potential to achieve improved flight performance across different flight conditions by changing its geometry according to changing flight conditions.
Yu Zhang +6 more
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Trailing-edge morphing wings have emerged as a promising solution for enhancing aerodynamic efficiency in low-Reynolds-number unmanned aerial vehicles (UAVs); however, their structural performance under large deformation and actuation-driven loading ...
Siddalingappa P Kodigaddi
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Morphological evolution of bird wings follows a mechanical sensitivity gradient determined by the aerodynamics of flapping flight. [PDF]
Rader JA, Hedrick TL.
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Flow Control around the UAS-S45 Pitching Airfoil Using a Dynamically Morphing Leading Edge (DMLE): A Numerical Study. [PDF]
Bashir M +4 more
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Asymmetric Airfoil Morphing via Deep Reinforcement Learning. [PDF]
Lu K, Fu Q, Cao R, Peng J, Wang Q.
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Effects of Speed on Coupled Sweep and Camber in Morphing Wings [PDF]
Lawren L. Gamble +2 more
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