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。
It is of great significance and difficulty to ensure the stability of the composite corrugated panels in the design of aircraft wing structures.
飞机机翼挂装翼尖导弹对机翼结构设计和结构分析提出了诸多全新课题， 如结构的振动响应和气动弹性动响应。
Missile carrying on the wing tip causes the wing structure design and analysis to face many challenges, such as structural vibration response and aeroelastic response.
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。
Ensuring the stability of the composite skin is of great significance in the design of aircraft wing structures.
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