翼肋（wing rib）：是飞机机翼的一个重要构成之一，机翼的横向受力骨架，一般与翼型的形状一致，用来支持飞机机翼的蒙皮，维持机翼的剖面形状。
为验证该算法，给出了一个飞机水平安定面翼肋设计实例。
To test this algorithm, one design example, one rib of an aircraft wing, is given.
使用有限体积法计算了飞行时的气动载荷，分析了前缘切口和翼肋开孔对压强分布的影响；
The finite volume method was used to compute the aerodynamic load, and the effect of leading-edge cut and ribs on the pressure distribution was analyzed simultaneously.
摘要 ：将拓扑优化设计技术应用到飞机的翼肋结构中，根据初始数模建立了该结构的拓扑优化模型。
Thepaper applied the topologyoptimization technology to Wing Rib Structure, and build the topologyoptimization model based its structure model.
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