并据此建立了原始疲劳质量符合性检查的EIF - SR判据和寿命判据。
Then EIFSR criterion and life criterion for initial fatigue quality evaluation and coincidence check are established.
本文介绍了一个定量地确定飞机结构细节(紧固孔)的原始疲劳质量的工程方法。
In this paper, an engineering approach for determining initial fatigue quality (IFQ) of aeronautic structure details (fastener holes) is introduced.
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