Abstract
The integral panel is significant structure of modern advanced aircraft. Stability is one of the most important problems of aircraft structure design. This paper focused on the compression properties of the material 7B50-T7751 and 7150-T7751. According to the engineering algorithm, we got the compression result of the wing integral panel. By the experimental study, we can obtain the load-strain curves of the two integral panel forms. The comparison of the compression properties provides a basis to the choice of integral panel.
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Schedule a callMore From: International Journal of Lightweight Materials and Manufacture
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