Unsteady aerodynamics of a morphing tandem-wing unmanned aerial vehicle

• المؤلفون الرئيسيون: Zhang, G. Q., Yu, S. C. M.
• مؤلفون آخرون: School of Mechanical and Aerospace Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2013
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/85676; http://hdl.handle.net/10220/11677
• المؤسسة: Nanyang Technological University

The effects of unsteady aerodynamics for a tandem-wing unmanned aerial vehicle (UAV) prototype during the morphing stage have been investigated numerically at low Reynolds numbers (Re<10^6). The morphing stage consists of two stages. The first stage involves the unfolding of the canards and wings...