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Least-squares, continuous sensitivity analysis for nonlinear fluid-structure interaction.

机译:最小二乘,连续灵敏度分析,用于非线性流固耦合。

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A least-squares, continuous sensitivity analysis method was developed for transient aeroelastic gust response problems to support computationally efficient analysis and optimization of aeroelastic design problems. A key distinction between the local and total derivative forms of the sensitivity system was introduced. The continuous sensitivity equations and sensitivity boundary conditions were derived in local derivative form which was shown to be superior for several applications. The analysis and sensitivity problems were both posed in a first-order form which is amenable to a solution using the least-squares finite element method. Several example and validation problems were presented and solved, including elasticity, fluid, and fluid-structure interaction problems. Significant contributions of the research include the first sensitivity analysis of nonlinear transient gust response, a local derivative formulation for shape variation that requires parameterizing only the boundary, and statement of sufficient conditions for using nonlinear "black box" software to solve the sensitivity equations. Promising paths for future investigation were presented and discussed.
机译:针对瞬态气动弹性阵风响应问题,开发了一种最小二乘连续灵敏度分析方法,以支持有效计算分析和优化气动弹性设计问题。引入了灵敏度系统的局部和全导数形式之间的关键区别。以局部导数形式导出了连续的灵敏度方程和灵敏度边界条件,这在某些应用中被证明是优越的。分析和灵敏度问题都以一阶形式提出,可以使用最小二乘有限元法求解。提出并解决了一些示例和验证问题,包括弹性,流体和流固耦合问题。该研究的重要贡献包括对非线性瞬态阵风响应的首次敏感性分析,仅需对边界进行参数化的局部变形公式(仅需对边界进行参数化处理),以及陈述了使用非线性“黑匣子”软件求解敏感性方程式的充分条件。提出并讨论了未来调查的可能途径。

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