Results 51 to 60 of about 311 (175)
This study employs the hybrid of electrolysis and fluidic reaction (HEFR) technique to investigate an experimental soft actuator model designed as an artificial myosin. Energy is generated through chemical reactions involving acetic acid (CH3COOH), bicarbonate (NaHCO3), and water (H2O), combined with chemical electrolysis, which powers the soft ...
Ramin Zakeri +2 more
wiley +1 more source
In numerical virtual flight (NVF) tasks, strong unsteady flow disturbances can change aerodynamic behavior and reduce the effectiveness of control surfaces, increase the difficulty of aerodynamics modeling and controlling at high‐angle‐of‐attack (high‐AoA).
Dongyu Zhao +5 more
wiley +1 more source
Unsteady Aerodynamics of Continuously Morphing Airfoils from Transonic to Hypersonic Regimes
Designing high-speed aircraft for wide-speed-range operation remains a major aerodynamic challenge. This study investigates the unsteady aerodynamics of a continuously morphing airfoil from transonic to hypersonic regimes. A smooth morphing trajectory is
Linyi Zhi +4 more
doaj +1 more source
Analysis of Energy Budget Characteristics of Three‐Segment Wings in Wind Gradient Dynamic Soaring
Wind gradient dynamic soaring enables bioinspired aerial vehicles to harvest environmental energy and extend endurance; yet quantitative comparisons remain scarce on how multisegment wing configurations translate, under identical control and wind field conditions, into differences in energy budget.
Yonggang Yang +2 more
wiley +1 more source
Modeling and control of a morphing airfoil structure
The aeroelastic modeling and robust control design for a morphing airfoil concept is presented. A finite dimensional linear time invariant aeroelastic model was developed for a multi-input, multi-output morphing airfoil structure. The shape of the airfoil (NACA airfoil series 2415) was controlled by actuators distributed along the top airfoil surface ...
openaire +3 more sources
Unmanned aerial vehicles (UAVs) with flying wing designs offer unique advantages in terms of maneuverability and fuel efficiency, but achieving precise control over these tailless aircraft can be challenging. This study investigates the potential of notch leading edge (NLG) technology to improve the effectiveness of control surfaces in flying wing UAVs.
Mohammad Hossein Moghimi Esfandabadi +2 more
wiley +1 more source
This paper investigates magnetic soft actuators for aerospace use. Various actuators with different magnetic particle fractions are created and tested to enhance their multifunctional performance, specifically displacement ability and mechanical strength, which significantly improved their mechanical strength by incorporating natural and synthetic ...
Diogo Santos +3 more
wiley +1 more source
A Data‐Driven Approach to Integrated Adaptive Morphing and Guidance for Cruise Missiles
ABSTRACT To address the complex coupling between aerodynamic characteristics and guidance control for morphing flight missiles, this study proposes a data‐driven approach to integrated adaptive morphing and guidance. Firstly, an aerodynamic surrogate model is constructed using a fully connected neural network (FCNN), mapping the configuration ...
Ming‐Yu Wu +6 more
wiley +1 more source
Aerodynamic enhancement of wind turbine blades through Peregrine falcon‐inspired surface designs
Abstract As global energy demands increase, enhancing renewable energy technologies, particularly wind turbines, is essential to meet sustainability goals. However, achieving higher efficiency remains challenging due to limitations in traditional blade designs. This study explores an innovative solution by applying biomimetic principles inspired by the
Yasin Furkan Gorgulu, Mustafa Arif Ozgur
wiley +1 more source
Abstract Subsurface geometries, such as faults and subducting slab interfaces, are often poorly constrained, yet they exert first‐order control on key geophysical processes, including subduction zone thermal structure and earthquake rupture dynamics.
Gabrielle M. Hobson +2 more
wiley +1 more source

