DOI | Resolve DOI: https://doi.org/10.2514/6.2016-4037 |
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Author | Search for: Koreanschi, Andreea; Search for: Oliviu, Sugar Gabor; Search for: Acotto, Joran; Search for: Botez, Ruxandra M.; Search for: Mamou, Mahmoud1; Search for: Mebarki, Youssef1 |
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Affiliation | - National Research Council of Canada. Aerospace
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Format | Text, Article |
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Conference | 34th AIAA Applied Aerodynamics Conference, June 13-17, 2016, Washington, D.C. |
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Abstract | In the present paper an ‘in-house’ genetic algorithm is described and applied to an
optimization problem of improving the aerodynamic performances of an airfoil through
upper surface morphing. The results of the optimization of the flow behavior for the airfoil
morphing upper-surface problem are validated with experimental transition results obtained
with Infra-red Thermography for the CRIAQ MDO 505 wing tip demonstrator, proving that
the 2D numerical optimization using the ‘in-house’ genetic algorithm is an important tool in
improving various aspects of a wing’s performances |
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Publication date | 2016-06-13 |
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Publisher | American Institute of Aeronautics and Astronautics |
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Place | Reston, Virginia |
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In | |
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Language | English |
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Peer reviewed | Yes |
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NPARC number | 23000695 |
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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 | dde71a65-95c5-4a04-af2f-7d2b47a44a6e |
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Record created | 2016-08-24 |
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Record modified | 2020-03-16 |
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