基于响应面全局优化技术的蜂窝板材料性能参数修正

Honeycomb sandwich plates are used widely in the aerospace industry. Building accurate finite element models of honeycomb sandwich plates is necessary for analyzing and optimizing the microvibration that occurs in spacecraft. A finite element dynamic model of a honeycomb plate was built, and then by using orthogonal design of experimental computation, the most important material parameters of honeycomb core equivalent model were identified. Through the global optimization based on adaptive sampling guided by response surface model, the parameters of honeycomb core were updated efficiently. The average error of first six modal frequencies of the updated finite element model against experimental result is reduced to less than 1%.