Structural Modelling of Compliance-Based Morphing Structures under Transverse Shear Loading
Author:
Affiliation:
1. University of Bristol
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0229
Reference36 articles.
1. A Review of Morphing Aircraft
2. Wind tunnel testing of the fish bone active camber morphing concept
3. Shape morphing of aircraft wing: Status and challenges
4. Performance Comparison between Optimised Camber and Span for a Morphing Wing
5. Parker, H. “The Parker Variable Camber,” Tech. Rep. 77, National Advisory Committee for Aeronautics, Washington, DC, 1920.
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1. Experimental Aerodynamic Comparison of Active Camber Morphing and Trailing-Edge Flaps;AIAA Journal;2021-07
2. Concept Investigation of a Lightweight Composite Lattice Morphing Wing;AIAA Journal;2021-06
3. Structural Modeling of Compliance-Based Camber Morphing Structures Under Transverse Shear Loading;AIAA Journal;2020-11
4. Numerically Efficient Three-Dimensional Fluid-Structure Interaction Analysis for Composite Camber Morphing Aerostructures;AIAA Scitech 2020 Forum;2020-01-05
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