Structural Modelling of Compliance-Based Morphing Structures under Transverse Shear Loading

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

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Abstract

A parametrically driven structural model based on Mindlin-Reissner plate theory is developed to capture the three-dimensional deformations of a compliance-based morphing trailing edge device with severe structural discontinuities. This model addresses limitations of a previously developed Kirchoff-Love plate model, where out-of-plane displacements under torsional loading could not be accurately predicted due to unmodelled transverse shear deformations. The model is used to study the Fish Bone Active Camber (FishBAC) device, which is modelled here as a discontinuous plate structure, which captures the sudden changes in stiffness created by the concept geometrical configuration. Courant’s penalty method is implemented in the form of artificial penalty springs, to account for stiffness discontinuities. A numerical validation is performed using Finite Element Analysis (FEA). This analytical model represents a robust, efficient, mesh-independent and parameter-driven solution to modelling discontinuous plate structures. These traits make it useful for ongoing fluid-structure interaction analysis and optimisation of the FishBAC concept, and for application to other complex composite structures.

Original languageEnglish
Title of host publicationAIAA Scitech 2019 Forum
Place of PublicationSan Diego, California
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages17
ISBN (Electronic)9781624105784
ISBN (Print)9781624105784
DOIs
Publication statusPublished - 6 Jan 2019
EventAIAA Scitech Forum, 2019 - San Diego, United States
Duration: 7 Jan 201911 Jan 2019
https://scitech.aiaa.org/

Publication series

NameAIAA Scitech 2019 Forum

Conference

ConferenceAIAA Scitech Forum, 2019
CountryUnited States
CitySan Diego
Period7/01/1911/01/19
Internet address

Structured keywords

  • Bristol Composites Institute ACCIS

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