...
机译:灵活性对悬停和向前飞行翼特性的影响
R&
D Strategy Team Vehicle &
Launcher System R&
D Division Hanwha Defense Systems;
Department of Aerospace Engineering;
BK21 Plus Transformative Training Program for Creative Mechanical and Aerospace Engineers Institute of Advanced Machines and Design Seoul National University 1 Gwanak-ro;
Department of Mechanical and Aerospace Engineering Institute of Advanced Aerospace Technology Seoul National University;
Fluid-structure interaction (FSI); Computational fluid dynamics (CFD); Computational structural dynamics (CSD); Aeroelasticity; Flapping wing;
机译:灵活性对悬停和向前飞行翼特性的影响
机译:扑翼微型飞机“ DelFly II”在悬停飞行中的力产生和机翼变形特性
机译:襟翼微空中飞行器从悬停到向前飞行的最佳过渡
机译:从悬停中被动稳定的拍打飞行,以快进通过机翼位置的转变
机译:悬停和向前飞行中襟翼的非线性近似气动弹性分析
机译:盘旋飞行中扑翼的三维涡流尾迹结构
机译:机翼灵活性对向前飞行中扑翼Mavs的飞行动力学稳定性的影响