An analytical approach is proposed to obtain the sensitivity of structural responses in aeroelastic tailoring.

进行了一种用解析方法求气动弹性剪裁中的结构响应值敏度的研究。

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Aeroelastic tailoring technique involves mechanics of composite materials, aeroelastic dynamics and optimization methods.

复合材料气动弹性剪裁技术涉及复合材料力学、气动弹性力学和优化方法。

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This paper comprehensively introduces a survey and a theory foundation concerning the aeroelastic tailoring for the present composite aircraft.

本文综合介绍了当前复合材料的飞机结构在气动弹性剪裁方面的概况及其理论基础。

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