A Dynamic Loading Mechanism for a Morphing Winglet
Author:
Affiliation:
1. Ryerson University Department of Aerospace Engineering, , 350 Victoria St, Toronto, ON M5B 2K3 , Canada
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
https://asmedigitalcollection.asme.org/mechanismsrobotics/article-pdf/15/5/054501/6950644/jmr_15_5_054501.pdf
Reference14 articles.
1. Winglet Multi-Objective Shape Optimization;Elham;Aerosp. Sci. Technol.,2014
2. Nonplanar Wing Concepts for Increased Aircraft Efficiency;Kroo,2005
3. Analysis and Control of an Actuation-Redundant Parallel Mechanism Requiring Synchronization;Xi;ASME J. Mech. Rob.,2020
4. Aerodynamic Analysis of Variable Cant Angle Winglets for Improved Aircraft Performance;Beechook,2013
5. Structural Testing and Analysis of a Joined Wing Technology Demonstrator
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