| DOI | Resolve DOI: https://doi.org/10.2514/6.2019-2352 |
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| Author | Search for: Fortin, Francois1; Search for: Renaud, Guillaume1; Search for: Roy, Steven1 |
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| Affiliation | - National Research Council of Canada. Aerospace
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| Format | Text, Article |
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| Conference | AIAA Scitech 2019 Forum, 7-11 January 2019, San Diego, CA, USA |
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| Subject | aviation; computational fluid dynamics; nanocomposites; Cfd approaches; low order; method of moving asymptotes; morphing; optimal shape; optimization approach |
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| Abstract | NRC is developing a technology demonstrator of a stretchable morphing leading edge. Shape optimization of two concepts of droop leading edge was performed using a low-order CFD approach with the Method of Moving Asymptotes optimization approach. A prototype demonstrator was built using the optimal shapes with a novel nanocomposite material and internal mechanism. This paper describes the aerodynamic part of the development. |
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| Publication date | 2019-01-06 |
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| Publisher | American Institute of Aeronautics and Astronautics |
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| In | |
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| Language | English |
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| Peer reviewed | Yes |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | b25bc054-8f59-478e-ae58-f2326eb6a083 |
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| Record created | 2021-08-24 |
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| Record modified | 2021-08-24 |
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