A combined numerical and experimental approach to investigations of body-freedom flutter on flying wings

• المؤلف الرئيسي: Ang, Elijah Hao Wei
• مؤلفون آخرون: Ng Bing Feng
• التنسيق: Thesis-Doctor of Philosophy
• اللغة: English
• منشور في: Nanyang Technological University 2024
• الموضوعات: Engineering; Aeroelasticity; Unmanned aerial vehicles; Body-freedom flutter; Wind tunnel; Gust load alleviation
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/173670
• المؤسسة: Nanyang Technological University

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...