This conclusion may provide experimental evidence for fatigue life prediction and design of titanium alloy wing main beam.
该结论可为机翼钛合金主梁构件疲劳寿命预测及疲劳设计提供试验依据。
This conclusion may provide experimental evidence for fatigue life prediction and design of titanium alloy wing main beam.
该结论可为机翼钛合金主梁构件疲劳寿命预测及疲劳设计提供试验依据。
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