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| AERO0016-3

 | Aeroelasticity

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| Duration : | 20h Th | |
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| Holder(s) : | Laurent Stainier | |
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| Course contents :
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- General introduction to aeroelastic phenomenae
- Static aeroelasticity: typical section concept, divergence, control surface efficiency.
- Dynamic aeroelasticity: unsteady aerodynamics and the Theodorsen function, flutter and solution methods.
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| Course objective :
| This course provides an introduction to aeroelasticity. It focuses more particularly on the main aeroelastic phenomenae (divergence, flutter, command inversion, lift redistribution) and describes the main semi-analytical solution methods used in linear aeroelasticity. | |
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| Prerequisites :
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- Introductory course in aerodynamics.
- Introductory course in structural dynamics.
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| Workshops :
| Topics developped in class will be applied through an integrated exercise (AERO0019-1) aiming at the design of an airplane wing. | |
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| Written notes :
| Class notes will be available online through MyULg. | |
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| Assessment :
| Oral exam. | |
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| Contacts :
| Laurent STAINIER
Institut de Mécanique (B52), +2/538
Tel: 04-366.91.52
E-mail: L.Stainier@ulg.ac.be | |
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