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Response of Damaged and Undamaged Tailored Extension-Shear-Coupled Composite Panels.

机译:受损和未损坏的剪切延伸 - 剪切耦合复合板的响应。

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摘要

The results of an analytical and experimental investigation of the response of composite I-stiffener panels with extension-shear coupling are presented. This tailored concept, when used in the panel cover skins of a tiltrotor aircraft wing has the potenti ...

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