Aeroelastic Flutter of Subsonic Aircraft Wing Section with Control Surface
Aeroelastic flutter in aircraft mechanisms is unavoidable, essentially in the wing and control surface. In this work a three degree-of-freedom aeroelastic wing section with trailing edge flap is modeled numerically and theoretically. FLUENT code based on the steady finite volume is used for the pred...
| Published in: | Journal of Engineering |
|---|---|
| Main Authors: | , , |
| Format: | Article |
| Language: | English |
| Published: |
University of Baghdad
2015-12-01
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| Subjects: | |
| Online Access: | http://joe.uobaghdad.edu.iq/index.php/main/article/view/292 |