Affiliation:
1. Naval Aeronautical and Astronautical Academy
Abstract
The mechanism of injury and damage evolution of composite aircraft is complex, traditional methods fatigue test relies on a large number of structural durability test data, not only consume large, but limited applicability. In order to ensure the fatigue of composite structures validated statistically, this article describes the most common methods: Life scatter factor method, load enhancement factor method and ultimate strength method.
Publisher
Trans Tech Publications, Ltd.
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