本文针对后缘变弯度机翼，设计出一种新的柔性蜂窝结构。
In this article, a new flexible honeycomb structure is designed for the wing with a variable camber trailing edge.
实现机翼在不同的飞行状态下的最优气动外形是变弯度自适应机翼的一项关键技术。
Making aircraft wing vary under different flying speeds is a key technology of variable camber adaptive wing.
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