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Wake Vortex Model for Real-Time Flight Simulation Based on Large Eddy Simulation

机译:基于大涡模拟的实时涡流尾迹涡模型

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摘要

An alternative approach is presented to represent a counter-rotating vortex pair for wake vortex interaction in a real-time flight simulation. Rather than using an analytical model, the model directly accesses a precomputed three-dimensional time-varying dataset. This dataset is generated using implicit large eddy simulations on unstructured grids. The methodology enables a realistic vortex decay to be reproduced with the apparition of short- and long-wave instabilities. The vortex model based on these simulations is designed to run on a personal computer and is integrated with a six-degree-of-freedom real-time flight simulator. The paper combines the use of large eddy simulation data as the basis of a wake vortex encounter model with methods to access the dataset in real time. The second half of this paper describes the data compression scheme implemented to reduce the size of the time-varying dataset. Additionally, rapid data access and issues regarding the real-time data management aspects are discussed. Analysis of the performance of the model is made and preliminary comparisons with a traditional analytical wake vortex model are discussed.
机译:提出了一种替代方法来表示实时飞行模拟中用于尾流涡流相互作用的反向旋转涡流对。该模型不使用分析模型,而是直接访问预先计算的三维时变数据集。该数据集是使用非结构化网格上的隐式大涡模拟生成的。该方法使短波和长波不稳定性表现出真实的涡旋衰减。基于这些模拟的涡流模型被设计为在个人计算机上运行,​​并与六自由度实时飞行模拟器集成在一起。本文将大型涡流模拟数据的使用(作为尾流涡流遭遇模型的基础)与实时访问数据集的方法相结合。本文的下半部分描述了为减少时变数据集的大小而实施的数据压缩方案。此外,还讨论了快速数据访问以及有关实时数据管理方面的问题。对该模型的性能进行了分析,并讨论了与传统解析尾流涡流模型的初步比较。

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