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研究了军用飞机在服役环境下的湿热谱和复合材料结构的湿扩散以及 相应的湿应力场，给出了某军用飞机模型复合材料机翼结构的分析数值结 果。所给出的分析方法和数值分析结论对军用飞机结构设计和分析工作者有 参考价值。
The wet heat spectrum of military aircraft under service environment and the wet diffusion of composite materials structure and the corresponding wet stress field were studied. The numerical results of the composite aircraft wing structure of a military aircraft model were given. The analytical methods and numerical analysis conclusions given are of reference value for military aircraft structural design and analysis workers.