Download | - View accepted manuscript: Morphing wing real time optimization in wind tunnel tests (PDF, 1.0 MiB)
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Author | Search for: Popov, Andrei Vladimir; Search for: Grigorie, Teodor lucian; Search for: Botez, Ruxandra Mihaela; Search for: Mamou, Mahmoud1; Search for: Mebarki, Youssef1 |
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Affiliation | - National Research Council of Canada. NRC Institute for Aerospace Research
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Format | Text, Article |
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Conference | ICINCO 2010, the 7th International Conference on Informatics in Control, Automation and Robotics, June 15-18, 2010, Funchal, Madeira, Portugal |
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Abstract | In this paper, wind tunnel results of a real time optimization of a morphing wing in wind tunnel for delaying the transition towards the trailing edge are presented. A morphing rectangular finite aspect ratio wing, having a wind tunnel experimental airfoil reference cross-section, was considered with its upper surface made of a flexible composite material and instrumented with Kulite pressure sensors, and two smart memory alloys actuators. Several wind tunnel tests runs for various Mach numbers, angles of attack and Reynolds numbers were performed in the 6'x9' wind tunnel at the Institute for Aerospace Research at the National Research Council Canada. Unsteady pressure signals were recorded and used as feed back in real time control while the morphing wing was requested to reproduce various optimized airfoils by changing automatically the two actuators strokes. The paper shows the optimization method implemented into the control software code that allows the morphing wing to adjust its shape to an optimum configuration under the wind tunnel airflow conditions. |
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Publication date | 2010 |
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Publisher | SciTePress, Science and Technology Publications |
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In | |
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Language | English |
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Peer reviewed | Yes |
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NPARC number | 23001288 |
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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 | 2ab3650a-db0c-4996-88e8-9ef8052aa3f5 |
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Record created | 2017-01-13 |
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Record modified | 2020-06-04 |
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