Results 41 to 50 of about 27,517 (135)

Residual Stress‐Driven Non‐Euclidean Morphing in Origami Structures

open access: yesAdvanced Intelligent Systems
Morphing origami has numerous potential engineering applications owing to its intrinsic morphing features from 2D planes to 3D surfaces. However, the current 1D hinge deformation‐driven transformation of foldable origami with rigid or slightly deformable
Zihe Liang   +6 more
doaj   +1 more source

Rigid–Elastic Coupling Dynamics of Morphing Wing Aircraft

open access: yesAerospace
This paper presents a rigid–elastic coupling dynamic model for a morphing aircraft with variable-sweep wings, developed using Kane’s method. The model accurately captures the interactions between flight dynamics and structural dynamics during morphing ...
Siyu Hua, Xugang Wang, Zhongyuan Wang
doaj   +1 more source

Feedforward Unsteady Lift Hysteresis Compensation of Variable Camber Wing Based on Prandtl–Ishlinskii Model

open access: yesMathematics
The maneuvering flight of future aircraft which employ morphing variable camber wings (VCWs) requires rapid and accurate aerodynamic regulation. However, the dynamic lift responses during fast morphing deflection exhibit unsteady hysteresis effects ...
Xiaoming Wang   +4 more
doaj   +1 more source

Multiobjective Optimization for the Aero-Structural Design of Adaptive Compliant Wing Devices

open access: yesApplied Sciences, 2020
The design of morphing structures must combine conflicting structural requirements and multiple load conditions that are related to the aerodynamic shapes aimed at optimizing aircraft performance.
Alessandro De Gaspari
doaj   +1 more source

SMART MORPHING CONCEPTS AND APPLICATIONS FOR ADVANCED LIFTING SURFACES [PDF]

open access: yes, 2009
The aim of this thesis has been the study and implementation of structural solutions for the local or global change of airplanes wing geometry (adaptive wing): they may lead to an increase in aerodynamic efficiency and reduced operating costs and ...
Barbarino, Silvestro
core   +2 more sources

SynMorph: Generating Synthetic Face Morphing Dataset With Mated Samples

open access: yesIEEE Access
Face morphing attack detection (MAD) algorithms have become essential to overcome the vulnerability of face recognition systems. To solve the lack of large-scale and public-available datasets due to privacy concerns and restrictions, in this work we ...
Haoyu Zhang   +3 more
doaj   +1 more source

Feature Interaction-Based Face De-Morphing Factor Prediction for Restoring Accomplice’s Facial Image

open access: yesSensors
Face morphing attacks disrupt the essential correlation between a face image and its identity information, posing a significant challenge to face recognition systems. Despite advancements in face morphing attack detection methods, these techniques cannot
Juan Cai   +4 more
doaj   +1 more source

Morphing Quadrotors: Enhancing Versatility and Adaptability in Drone Applications—A Review

open access: yesDrones
The advancement of drone technology has underscored the critical need for adaptability and enhanced functionality in unmanned aerial vehicles (UAVs). Morphing quadrotors, capable of dynamically altering their structure during flight, offer a promising ...
Siyuan Xing   +5 more
doaj   +1 more source

Correcting Position Error in Precipitation Data Using Image Morphing

open access: yesRemote Sensing, 2019
Rainfall estimates based on satellite data are subject to errors in the position of the rainfall events in addition to errors in their intensity. This is especially true for localized rainfall events such as the convective rainstorms that occur during ...
Camille Le Coz   +4 more
doaj   +1 more source

Static Aeroelastic Characteristics of Morphing Trailing-Edge Wing Using Geometrically Exact Vortex Lattice Method

open access: yesInternational Journal of Aerospace Engineering, 2019
A morphing trailing-edge (TE) wing is an important morphing mode in aircraft design. In order to explore the static aeroelastic characteristics of a morphing TE wing, an efficient and feasible method for static aeroelastic analysis has been developed in ...
Sen Mao   +3 more
doaj   +1 more source

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