气动弹性
颤振
模式(计算机接口)
结构工程
翼型
空气动力学
控制理论(社会学)
航空航天工程
计算机科学
工程类
操作系统
人工智能
控制(管理)
作者
Bret Stanford,Andrew S. Thelen,Kevin Jacobson
出处
期刊:AIAA Journal
[American Institute of Aeronautics and Astronautics]
日期:2024-09-25
卷期号:: 1-9
摘要
Aeroelastic flutter design derivatives may be approximated by ignoring the sensitivity of the structural mode shapes. This fixed-mode derivative is less expensive to compute than the exact free-mode derivative (which accommodates the mode shape dependency) but also may provide inaccurate sensitivities for optimization. This work formulates both fixed- and free-mode flutter derivatives and demonstrates the conditions under which they are equivalent. Two different types of fixed-mode derivatives are also developed in this work. Using a cantilevered-plate demonstration problem with both shape and sizing design parameters, the accuracy of the free-mode derivative and the two fixed-mode derivatives is demonstrated via gradient-based optimization.
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