HDO divides the integrated optimization of composite wing structures into two sub-problems that are easy to be solved: upper level optimization and lower level optimization.
它将复合材料翼面结构综合优化设计问题分解成两个易于求解的子问题：顶层优化设计和底层优化设计。
Ensuring the stability of the composite skin is of great significance in the design of aircraft wing structures.
复合材料蒙皮稳定性是飞机翼面结构设计需要考虑的重要方面。
It is of great significance and difficulty to ensure the stability of the composite corrugated panels in the design of aircraft wing structures.
复合材料波纹板稳定性是飞机机翼结构设计需要考虑的重要方面，是目前飞机结构设计中的一大难点。
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