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...
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| Главные авторы: | , , |
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| Формат: | Artigo |
| Язык: | Inglês |
| Опубликовано: |
University of Baghdad
2015-12-01
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| Серии: | Journal of Engineering |
| Предметы: | |
| Online-ссылка: | http://joe.uobaghdad.edu.iq/index.php/main/article/view/292 |
| Метки: |
Нет меток, Требуется 1-ая метка записи!
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