Results 41 to 50 of about 748 (184)

Continuous morphing camber for aerodynamic surfaces

open access: yes, 2023
reservedSin dagli albori, l’uomo ha cercato di imitare ed ispirarsi alla natura in ogni ambito artistico e tecnico. Ne è un esempio il fascino e l’interesse che il genere umano ha riservato e riserva riguardo il volo degli uccelli, i quali sono in grado
MICOLI, FRANCESCO
core  

Design and Shape Monitoring of a Morphing Wing Trailing Edge

open access: yesAerospace, 2023
The morphing wing trailing edge is an attractive aviation structure due to its shape-adaptive ability, which can effectively improve the aerodynamic performance of an aircraft throughout the whole flight.
Xintong Shi   +5 more
doaj   +1 more source

Magnetothermal‐Triggered Response and Self‐Healing of Recyclable and Reprocessable Nanocomposites for Actuation Systems

open access: yesAdvanced Functional Materials, Volume 36, Issue 45, 5 June 2026.
Developing recyclable materials for magnetic robotics that combine rapid response and self‐healing properties is challenging. Hence, this study focuses on the integration of magnetothermal nanoparticles into a dynamic sorbitol‐based vitrimer, a recyclable composite capable of remote actuation and self‐healing by magnetic heating.
Maria Weißpflog   +3 more
wiley   +1 more source

Kinematic Simulation and Structure Analysis of a Morphing Flap [PDF]

open access: yes, 2013
This thesis presents a study on the design and analysis of a morphing flap structure integrated with actuation mechanism for potential application to large aircraft.
Guo, Shixian
core  

Impacts of Blade Camber on Cross‐Flow Turbine Performance and Loading

open access: yesWind Energy, Volume 29, Issue 5, May 2026.
ABSTRACT Cross‐flow turbines show promise for renewable energy generation from wind and tidal sources. The rotating reference frame of cross‐flow turbine blades results in virtual camber and incidence due to streamline curvature, altering the lift, drag, and pitching moment of the blades. Adding geometric camber is therefore likely to alter performance
Ari Athair   +3 more
wiley   +1 more source

Analysis of composite wing structures with a morphing leading edge [PDF]

open access: yes, 2011
One of the main challenges for the civil aviation industry is the reduction of its environmental impact. Over the past years, improvements in performance efficiency have been achieved by simplifying the design of the structural components and using ...
Morishima, Ryoko
core  

Active Fluid Gurney Flaps, Controllable Lift Enhancement Toward Wind Turbine Power Production Regulation

open access: yesWind Energy, Volume 29, Issue 1, January 2026.
ABSTRACT Meeting the rising demand for renewable energy requires innovative solutions to enhance wind power extraction, particularly given demographic and geographic constraints on wind farm deployment. Active high‐lift devices, such as the Active Fluid Gurney Flap (AFGF), offer a promising approach that can dynamically modify aerodynamic performance ...
Mario Lucas, Jorge Saavedra
wiley   +1 more source

Design and Validation of a Passive Camber Morphing Concept for Rotorcraft

open access: yesAIAA SCITECH 2022 Forum, 2022
This paper presents an overview of the design and validation of a novel passive camber morphing system for rotorcraft. The passive system works for a variable speed rotor where a potential increase in pilot control authority and power reduction is possible.
Yasir Zahoor   +3 more
openaire   +3 more sources

Analysis of Energy Budget Characteristics of Three‐Segment Wings in Wind Gradient Dynamic Soaring

open access: yesInternational Journal of Aerospace Engineering, Volume 2026, Issue 1, 2026.
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

Optimal design of a composite active aeroelastic wing [PDF]

open access: yes, 2011
The primary aim of this research was to design a Seamless Aeroelastic Wing (SAW) structure applicable to a lightweight Unmanned Aerial Vehicle (UAV). Therefore the study focused on optimal design of a SAW structure by utilising the maximum aeroelastic ...
Perera, Melanie
core  

Home - About - Disclaimer - Privacy