A fatigue failure criterion of the unidirectional laminate was established based on both the residual strength degradation model and the plastic formula of anisotropy materials proposed by Hill method.

 
  • 在剩余強度衰減模型和希爾提出的各向異性材料塑性條件基礎上建立單向層合板在任意應力狀態(tài)下的疲勞破壞準則
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