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基于Ko位移理论的变体结构大变形精确重构方法研究

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摘要 变体飞行器是指机翼在翼展、面积、弦长等几何结构尺寸方面发生显著变化,使得飞行环境在大范围内(比如巡航、极高速飞行、快速俯冲、大迎角机动等)变化时,可以实现机翼外形和表面结构的重组,以适应监测到的飞行条件变化,获得最佳的气动和气弹特性(图1)。理想的变体机翼应当能够感知周围的环境,并且调整形状以便在各种不同的飞行条件下优化运行。
作者 王敏 徐志伟
出处 《江苏航空》 2020年第4期12-16,共5页 Jiangsu Aviation
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