Abstract
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 problem by coupling a geometrically nonlinear structural model to a potential flow aerodynamic model. The structure of the framework and the methodology used for the design of a morphing UAV wing are detailed. This wing is the focus of the European FP7 CHANGE project and serves as an example of the application of this methodology.
Original language | English |
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Title of host publication | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624103681 |
Publication status | Published - 1 Jan 2015 |
Externally published | Yes |
Event | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015 - Dallas, United States Duration: 22 Jun 2015 → 26 Jun 2015 |
Conference
Conference | 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015 |
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Country/Territory | United States |
City | Dallas |
Period | 22/06/15 → 26/06/15 |