Results 61 to 70 of about 1,860 (214)
Use of MDO Techniques for the Design of Morphing Aircraft [PDF]
, 2021 This paper describes the application of multidisciplinary optimization techniques to the design of adaptive morphing wings based on compliant structures.
Ricci S., Cavalieri V., De Gaspari A.
core +1 more source
Dynamic Model and Analysis of Asymmetric Telescopic Wing for Morphing Aircraft
MATEC Web of Conferences, 2016 Morphing aircraft has been the research hot topics of new concept aircrafts in aerospace engineering. Telescopic wing is an important morphing technology for morphing aircraft.
Chen Lili, Guo Zheng, Wang Wenkai
doaj +1 more source
Design of a Variable-Stiffness Compliant Skin for a Morphing Leading Edge
Applied Sciences, 2021 A seamless and smooth morphing leading edge has remarkable potential for noise abatement and drag reduction of civil aircraft. Variable-stiffness compliant skin based on tailored composite laminate is a concept with great potential for morphing leading ...
Zhigang Wang, Yu Yang
doaj +1 more source
Subterranean Mine Inspection Using the Prometheus Re‐Configurable Drone
Journal of Field Robotics, Volume 43, Issue 3, Page 1646-1660, May 2026.ABSTRACT This paper describes the design, development, and real‐world testing of an autonomous drone for subterranean exploration, known as “Prometheus.” Driven by requirements from industry that the drone be able to be deployed through areas of restricted access, Prometheus was designed to be directly deployed through a 150 mm aperture.
Liam Brown +8 more
wiley +1 more source
Dynamic Response and Pitch Damper Design for a Moderately Flexible, High-Aspect Ratio Aircraft [PDF]
, 2015 TCC (graduação) - Universidade Federal de Santa Catarina. Campus Joinville. Engenharia Aeroespacial.This work presents the dynamic response of a slightly flexible hight-aspect-ratio aircraft in time domain and the design of a pitch damper controller to ...
Lebkuchen, Hermann Luis
core
International Journal of Aerospace Engineering, 2019 In the present work, the aerodynamic shape design of an advanced high-lift system for a natural laminar flow (NLF) wing, based on the combination of a morphing droop nose and a single slot trailing edge flap, is presented.
Alessandro De Gaspari, Frédéric Moens
doaj +1 more source
Advanced Science, Volume 13, Issue 24, 27 April 2026.This review provides a comprehensive exploration of microstructure regulation strategies for multi‐principal element alloy‐based films and coatings, with a focus on the interplay between elemental composition, nanoscale architecture, heterostructures and interfacial engineering in tailoring their properties and functions. A systematic analysis of their
Jiaming Cao +4 more
wiley +1 more source
Optimization of a Composite Wing Subject to Multi Constraints [PDF]
, 2013 In this thesis, an investigation has been carried out into a minimum weight optimization analysis of a composite wing with multi design constraints under both static and dynamic loadings. The study includes the influence of a morphing leading edge on the
Fu, Qiang
core
Switching LPV control design with MDADT and its application to a morphing aircraft [PDF]
, 2016 summary:In flight control of a morphing aircraft, the design objective and the dynamics may be different in its various configurations. To accommodate different performance goals in different sweep wing configurations, a novel switching strategy, mode ...
Lü, Yongxi +9 more
core +1 more source
Roadmap on Artificial Intelligence‐Augmented Additive Manufacturing
Advanced Intelligent Systems, Volume 8, Issue 4, April 2026.This Roadmap outlines the transformative role of artificial intelligence‐augmented additive manufacturing, highlighting advances in design, monitoring, and product development. By integrating tools such as generative design, computer vision, digital twins, and closed‐loop control, it presents pathways toward smart, scalable, and autonomous additive ...
Ali Zolfagharian +37 more
wiley +1 more source