Spatially distributed load on aircraft structures is difficult to obtain due to the limitation of measurement technology, the complexity of load and the external environment of the aircraft during ...

中文翻译：

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基于子区域插值法的不规则平面结构分布式动荷载识别

由于测量技术的限制、载荷的复杂性以及飞行过程中飞行器的外部环境，飞机结构上的空间分布载荷难以获得。