A combined numerical and experimental approach to investigations of body-freedom flutter on flying wings
With the recent rise in the development of aircrafts with high aspect-ratio wings adopting lightweight flexible structures, these aircrafts become increasingly vulnerable to aeroelastic phenomena. One such example is flutter, a self-excited instability resulting from the coupling between inertial, s...
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| 格式: | Thesis-Doctor of Philosophy |
| 語言: | English |
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Nanyang Technological University
2024
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| 在線閱讀: | https://hdl.handle.net/10356/173670 |
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| 機構: | Nanyang Technological University |
| 語言: | English |