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High-fidelity methods for the prediction of ice debris trajectories

机译:高保真方法预测冰屑轨迹

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Ice release is of concern to aircraft manufacturers due to the potential damage that the ice debris can cause on aircraft components. This raises the need for accurate ice trajectory simulation tools to support pre-design, design and certification phases while improving cost efficiency. High-fidelity models involve fully coupled time-accurate aerodynamic and flight mechanics simulations and thus require the use of emerging simulation tools, such as approaches based on immersed boundary methods or chimera grids. In this paper, the developments of current simulations tools for ice block trajectories performed in the scope of the recently completed research project STORM are described and validated against a STORM experimental data base of trajectories created by the German Aerospace Center (DLR) in collaboration with the German-Dutch Wind Tunnel foundation.
机译:由于碎冰可能对飞机部件造成潜在的损坏,因此飞机制造商需要考虑冰的释放。这增加了对精确的冰轨迹模拟工具的需求,以支持预设计,设计和认证阶段,同时提高成本效率。高保真模型涉及时间精确的空气动力学和飞行力学仿真的完全耦合,因此需要使用新兴的仿真工具,例如基于沉浸边界方法或嵌合网格的方法。在本文中,描述了在最近完成的研究项目STORM范围内执行的冰块轨迹模拟工具的开发,并根据德国航空航天中心(DLR)与德国航天中心合作创建的轨迹的STORM实验数据库进行了验证。德荷风洞基金会。

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