Results 81 to 90 of about 748 (184)

High-Bandwidth Morphing Actuator for Aeroelastic Model Control

open access: yesAerospace, 2019
The design and testing of a high-bandwidth continuous actuator for aeronautical applications is presented hereinafter. The actuator has a dual goal of controlling both the aeroelastic behaviour and the flight mechanics of the model in which it is ...
Sebastiano Fichera   +2 more
doaj   +1 more source

Optimization shape design and realization of variable camber wing based on compliant mechanisms

open access: yes, 2023
DOTTORATOCamber morphing aircraft actively change their geometric configurations with different missions and flight conditions to achieve potential aerodynamic performance improvements, which is of significant interest to the aviation community.
Zhang, Zhenkai
core  

Construction of a Morphing Wing Rib Actuated by a NiTi Wire

open access: yesJournal of Aerospace Technology and Management, 2015
The main goal of this paper is to analyze if it is feasible to employ a trained shape memory alloy wire as a linear actuator to modify the camber of a morphing wing rib.
Thais Campos de Almeida   +2 more
doaj  

Morphing of ‘flying’ shapes for autonomous underwater and aerial vehicles

open access: yes, 2009
Autonomous vehicles are energy poor and should be designed to minimise the power required to propel them throughout their mission. The University of Southampton’s School of Engineering Sciences is actively involved in the development of improved designs ...
Nicholls-Lee, R.F.   +4 more
core  

Optimal design of an aeroelastic wing structure with seamless control surfaces [PDF]

open access: yes, 2009
This article presents an investigation into the concept and optimal design of a lightweight seamless aeroelastic wing (SAW) structure for small air vehicles.
M Perera   +3 more
core   +1 more source

Design and Analysis of a Novel Mechanism for the Morphing of Trailing Edge of an Aircraft Wing

open access: yesMATEC Web of Conferences, 2018
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
doaj   +1 more source

Aero-Structural Optimization and Performance Evaluation of a Morphing Wing with Variable Span and Camber

open access: yes, 2011
An aero-structural design and analysis study of a telescopic wing with a conformal camber morphing capability is presented. An aerodynamic analysis of a telescoping wing, first with a high speed airfoil followed by an analysis with a low speed airfoil ...
F. Lau, J. Vale, A. Suleman, A. Leite
core   +1 more source

Lifting-Line Predictions for the Ideal Twist Effectiveness of Spanwise Continuous and Discrete Control Surfaces

open access: yesApplied Sciences
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
doaj   +1 more source

Application of the Active Camber Morphing Concept Based on Compliant Structures to a Regional Aircraft

open access: yes, 2014
The present work addresses the optimal design of a morphing mechanism based on compliant structures used to implement the active camber morphing concept.
Sergio Ricci   +3 more
core   +1 more source

FLUTTER CONTROL OF AN AIRFOIL WITH CAMBER MORPHING NEAR GROUND

open access: yes, 2023
This paper presents the numerical investigation of the flutter control via the camber morphing of an airfoil under the ground effect. An aircraft experience a significant change in the aerodynamic characteristics while flying near the ground due to the ...
Dhital, Kailash   +2 more
core  

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