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本文介绍了在民用飞机制造过程中产生结构偏离时,对常见的偏离问题采取有限元强度分析,通过分析计算表明不同的多余空孔需要采取不同的处理方法。
This paper introduces the structural deviation in the manufacture of civil aircraft, the finite element strength analysis of the common deviation problem, analysis and calculation shows that different extra holes need to take a different approach.