机译:柔性铰接翼无尾微型飞行器的动力学和性能
Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana, Illinois 61801;
Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana, Illinois 61801;
Department of Aerospace Engineering University of Illinois at Urbana-Champaign, Urbana, Illinois 61801;
Department of Aerospace Engineering Wichita State University, Wichita, Kansas 67260;
b,c: wing span and chord length; D, L, Y: drag, lift, and side force; E, G: Young's modulus and modulus of rigidity of a material; I_b,I_p,(J): second moment of area about the in-plane axis along the direction of bending, polar moment of area, and torsional stiffness of a cross section of the wing; J_R,J_L,J: moment of inertia tensor of the right and left wings and the aircraft body, respectively, in the aircraft body frame; et al;
机译:蝙蝠风格瓦楞纸翼无人机车辆的设计,空气动力学分析和试验飞行
机译:具有机翼行程平面调制的生物启发性尾部扑翼微空气车的开发和飞行性能
机译:柔性扑翼微型飞行器气动特性的准稳态分析
机译:利用自适应柔性翼尖尖概念来优化积云微鸟空气动力学
机译:柔性机翼微型飞行器分布式参数系统升沉动力学建模与控制。
机译:跨翼微型空中航空车辆刚度设计的批量生料坯纺厂制造工艺
机译:柔性铰接翼无尾微型飞行器的动力学和性能
机译:柔性翼基微型飞行器:微型飞行器可控性评估。