Results 11 to 20 of about 2,244,717 (304)

Design and Analysis of Flexible Wing

open access: yesACS Journal for Science and Engineering, 2023
Modern transport aircrafts are introducing high lift devices to overcome the contradiction between economic considerations and low flight speed lift requirements. The flaps are known as high lifting devices.
Akhil P Thomas   +3 more
semanticscholar   +1 more source

Fluid–Structure Coupling and Aerodynamic Performance of a Multi-Dimensional Morphing Wing with Flexible Metastructure Skin

open access: yesAerospace, 2023
A multi-dimensional morphing wing skeleton mechanism is proposed with double-sided triangular pyramid units, which can realize continuous variable span-wise bend, span-wise twist, and sweep.
Hui Yang   +3 more
doaj   +1 more source

Static aeroelastic analysis of very flexible wings coupled with distributed propellers

open access: yesXibei Gongye Daxue Xuebao, 2023
Distributed propellers are widely used as propulsion for high-aspect-ratio long-endurance UAVs, and their load and slipstream will change the structural and aerodynamic characteristics of the wing, making geometric nonlinear effects more prominent.
WU Xuan, ZHOU Zhou, WANG Zhengping
doaj   +1 more source

Simulated pilot-in-the-loop testing of handling qualities of the flexible wing aircraft

open access: yesAviation, 2020
This article aims to indicate the differences between rigid and flexible wing aircraft flying (FQ) and handling (HQ) qualities. The Simulation Framework for Flexible Aircraft was used to provide a generic cockpit environment and a piloted mathematical ...
Vilius Portapas, Alastair Cooke
doaj   +1 more source

Numerical investigation of an insect-scale flexible wing with a small amplitude flapping kinematics

open access: yesThe Physics of Fluids, 2022
To maintain flight, insect-scale air vehicles must adapt to their low Reynolds number flight conditions and generate sufficient aerodynamic force. Researchers conducted extensive studies to explore the mechanism of high aerodynamic efficiency on such a ...
Yueyang Guo   +3 more
semanticscholar   +1 more source

Online Model-Free Reinforcement Learning for the Automatic Control of a Flexible Wing Aircraft [PDF]

open access: yesIET Control Theory & Applications, 2020
The control problem of the flexible wing aircraft is challenging due to the prevailing high non-linear deformations in the flexible wing system. This urged for new control mechanisms that are robust to the real-time variations in the wing's aerodynamics.
M. Abouheaf, W. Gueaieb, F. Lewis
semanticscholar   +1 more source

Aeroelastic Characterization of a Flexible Wing Using Particle Tracking Velocimetry Measurements

open access: yesAIAA Journal, 2021
The aerodynamic, elastic, and inertial components in Collar’s triangle of forces acting on a flexible wing with span width s=1.75  m and chord c=0.25  m are determined based on integrated optical m...
C. Mertens   +4 more
semanticscholar   +1 more source

Guidance Mechanism for Flexible-Wing Aircraft Using Measurement-Interfaced Machine-Learning Platform [PDF]

open access: yesIEEE Transactions on Instrumentation and Measurement, 2020
The autonomous operation of flexible-wing aircraft poses theoretical and technical challenges not yet addressed in the literature. The lack of an exact modeling framework is due to the complex nonlinear aerodynamics driven by the deformations of the ...
M. Abouheaf   +3 more
semanticscholar   +1 more source

Multidisciplinary Design and Optimization of Variable Camber Wing with Non-Equal Chord

open access: yesAerospace, 2023
Since the taper ratio of most wings is not equal to 1, the beam-disk trailing edge deflection mechanism originally designed for the rectangular wing is not fully applicable to the non-equal chord wing.
Yu Wang   +3 more
doaj   +1 more source

Identification and assessment of a nonlinear dynamic actuator model for controlling an experimental flexible wing

open access: yesCEAS Aeronautical Journal, 2021
In this paper, the effect of nonlinear actuator dynamics on the performance of an active load alleviation system for an experimental flexible wing is studied.
M. Tang   +3 more
semanticscholar   +1 more source

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