A Multi Fidelity Multi Disciplinary Analysis Optimization Framework for the Design of Morphing UAV Wings

Date

2015-06-22

Author

Ciarella, Andrea
Christos, Tsotskas
Hahn, Marco
Werter, Noud Pm
De Breuker, Roeland
Beaverstock, Chris
Friswell, Michael I
Yang, Yosheph
Özgen, Serkan
Antoniadis, Antonios
Tsoutsanis, Panagiotis
Drikakis, Dimitris

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https://hdl.handle.net/11511/74572

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A multi-fidelity, multi-disciplinary analysis and optimization framework for the design of morphing UAV wings Ciarella, Andrea; Tsotskas, Christos; Hahn, Marco; Werter, Noud P. M.; De Breuker, Roeland; Beaverstock, Chris S.; Friswell, Michael I.; Yang, Yosheph; Özgen, Serkan; Antoniadis, Antonios; Tsoutsanis, Panagiotis; Drikakis, Dimitris (null; 2015-01-01) © 2015 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.A framework for the design and optimization of a morphing wing is presented. It allows the user to simplify the design process of a morphing UAV wing with a simple and effective interface with the possibility to easily switch between flight phases and morphing concepts. It consists of two main solvers: a high-fidelity CFD module for detailed RANS simulation and a fast low-fidelity module that solves the aeroelastic prob...
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Citation Formats

A. Ciarella et al., “A Multi Fidelity Multi Disciplinary Analysis Optimization Framework for the Design of Morphing UAV Wings,” 2015, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/74572.