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Analysis of Aerodynamic Indices for Racing Sailing Yachts: a Computational Study and Benchmark on up to 128 CPUs

机译:赛车帆船游艇空气动力学指数分析:高达128 CPU的计算研究和基准

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This work presents a feasibility study for trustable and affordable CFD analysis of aerodynamic indices of racing sailing yachts. A detailed reconstructed model of a recent America's Cup class mainsail and asymmetrical spinnaker under light wind conditions has been studied using massive parallel RANS modeling on 128 CPUs. A detailed comparison between computational and experimental data has been performed and discussed, thanks to wind tunnel tests performed with the same geometry under the same wind conditions. The computational grid used was of about 37 millions of tetrahedra and the parallel job has been performed on up to 128 CPUs of a distributed memory Linux cluster using a commercial CFD code. An in deep analysis of the CPU usage has been performed during the computation by means of Ganglia and a complete benchmark of the studied case has been done for 64,48, 32, 16, 8 and 4 CPUs analyzing the advantages offered by two kind of available interconnection technologies: Ethernet and Infiniband. Besides to this computational benchmark, a sensitivity analysis of the global aerodynamic force components, the lift and the drag, to different grid resolution size has been performed. In particular, mesh size across three orders of magnitude have been investigated: from 0.06 million up to 37 million cells. The computational results obtained here are in great agreement with the experimental data. In particular, the fully tetra-hedral meshes allow appreciating the beneficial effect of the increasing of the grid resolution without changing grid topology: a converging trend to the experimental value is observed. In conclusion, the present results confirm the validity of RANS modeling as a design tool and show the advantages and costs of a large tetrahedral mesh for downwind sail design purposes.
机译:这项工作为赛车帆船游艇的空气动力学指数提供了可行性和实惠的CFD分析。在128CCU上的大规模平行RAN模型研究了最近的美洲杯类主帆和不对称纺纱机下的详细的重建模型。由于在相同风条件下的相同几何形状执行的风洞测试,已经执行和讨论了计算和实验数据之间的详细比较。所使用的计算网格具有约37百万四个四面体,并且使用商业CFD代码对多达128个CPU进行了平行作业。在通过Ganglia计算期间已经在计算期间进行了深入分析CPU使用率,并且已经为64,48,32,16,8和4 CPU进行了研究的完整基准,分析了两种提供的优势可用的互连技术:以太网和Infiniband。此外,已经执行了对该计算基准,已经进行了全局空气动力分量,电梯和拖曳到不同网格分辨率的敏感性分析。特别地,研究了三个数量级的网格尺寸:从0.06亿到3700万个细胞。这里获得的计算结果与实验数据非常一致。特别地,完全四HEDRAL网格允许欣赏栅格分辨率的增加而不改变网格拓扑的有益效果:观察到实验值的会聚趋势。总之,目前的结果证实了RAN建模作为设计工具的有效性,并显示了大型四面体网格用于下行风帆设计目的的优点和成本。

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