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首页> 外文期刊>Procedia Computer Science >Toward a Computational Steering Framework for Large-Scale Composite Structures Based on Continually and Dynamically Injected Sensor Data
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Toward a Computational Steering Framework for Large-Scale Composite Structures Based on Continually and Dynamically Injected Sensor Data

机译:基于连续动态注入的传感器数据的大型复合结构计算指导框架

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Recent advances in simulation, optimization, structural health monitoring, and high-performance computing create a unique opportunity to combine the developments in these fields to formulate a Dynamics Data Driven Application System (DDDAS) framework. In this paper we propose such a framework, which consists of the following items and features: a structural health monitoring (SHM) system, an advanced fluid—structure interaction (FSI) simulation module, and a sensitivity analysis, optimization and control software module. High-performance computing (HPC) is employed for the various parts of the framework and is viewed as its essential element. The intended application of the developed framework is the analysis of medium-to-large-scale composite structures. These include aerospace structures, such as military aircraft fuselage and wings, helicopter blades, and unmanned aerial vehicles, and civil structures, such as wind turbine blades and towers. The proposed framework will continuously and dynamically integrate the SHM data into the FSI analysis of these structures. This capability allows one to: 1. Shelter the structures from excessive stress levels during operation; 2. Make informed decisions to perform structural maintenance and repair; and 3. Predict the remaining fatigue life of the structure.
机译:在仿真,优化,结构健康状况监视和高性能计算方面的最新进展创造了独特的机会,可以结合这些领域的发展来制定动态数据驱动的应用系统(DDDAS)框架。在本文中,我们提出了这样一个框架,该框架包括以下各项和功能:结构健康监测(SHM)系统,高级流体-结构相互作用(FSI)模拟模块以及灵敏度分析,优化和控制软件模块。高性能计算(HPC)用于框架的各个部分,并被视为其基本要素。所开发框架的预期应用是对中大型复合结构的分析。这些包括航空航天结构,例如军用飞机的机身和机翼,直升机叶片和无人飞行器,以及民用结构,例如风力涡轮机的叶片和塔。拟议的框架将连续动态地将SHM数据集成到这些结构的FSI分析中。这种能力允许:1.在操作过程中保护结构免受过大的应力; 2.做出明智的决定以进行结构维护和修理; 3.预测结构的剩余疲劳寿命。

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