Topology Synthesis of Distributed Actuation Systems for Morphing Wing Structures

Journal of Aircraft - United States
doi 10.2514/1.25535
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

Fuzzy Logic Control of a Smart Actuation System in a Morphing Wing

2012English

Synthesis and Static Analysis of the Deployable Frame for a Morphing Wing

Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science
Mechanical Engineering
2012English

Span Morphing Using the GNATSpar Wing

Aerospace Science and Technology
Aerospace Engineering
2016English

Pressure Deflection Behavior of Candidate Materials for a Morphing Wing

English

Earth Mover’s Morphing: Topology-Free Shape Morphing Using Cluster-Based EMD Flows

Lecture Notes in Computer Science
Computer ScienceTheoretical Computer Science
2011English

Development and Testing of Woven FRP Flexure Hinges for Pressure-Actuated Cellular Structures With Regard to Morphing Wing Applications

Aerospace
Aerospace Engineering
2019English

Morphing Inflatable Wing Development for Compact Package Unmanned Aerial Vehicles

2004English

Topology Design of Pressure Adaptive Honeycomb for a Morphing Fowler Flap

2011English

Knowledge-Based Shape Optimization of Morphing Wing for More Efficient Aircraft

International Journal of Aerospace Engineering
Aerospace Engineering
2015English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy