Abstract
Structural elements made of carbon-filled plastics T700, T800, T1000, VKU-27l, and VKU-30KR14 535 are subjected to cyclic tensile and compressive tests. The relation between fatigue curve equation parameters is revealed. The results obtained for aviation alloys earlier are used to develop a general algorithm for predicting the fatigue life of an aviation construction in estimating its operational life characteristics.
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