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Axial-Flow Ventilation Fan Design Through Multi-Objective Optimization to Enhance Aerodynamic Performance

机译:通过多目标优化设计的轴流通风风扇以增强空气动力学性能

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This paper presents an optimization procedure for axial-flow ventilation fan design through a hybrid multiobjective evolutionary algorithm (MOEA) coupled with a response surface approximation (RSA) surrogate model. Numerical analysis of a preliminary fan design is conducted by solving three-dimensional (3-D) Reynolds-averaged Navier-Stokes (RANS) equations with the shear stress transport (SST) turbulence model. The multiobjective optimization processes are performed twice to understand the coupled effects of diverse variables. The first multiobjective optimization process is conducted with three design variables defining stagger angles at the hub, mid-span, and tip, and the second is conducted with five design variables defining hub-to-tip ratio, hub cap installation distance, hub cap ratio, and the stagger angles at the mid-span and tip. Two aerodynamic performance parameters, the total efficiency and total pressure rise, are selected as the objective functions for optimization. These objective functions are numerically assessed through 3-D RANS analysis at design points sampled by Latin hypercube sampling in the design space. The optimization yields a maximum increase in efficiency of 1.8percent and a 31.4percent improvement in the pressure rise. The off-design performance is also improved in most of the optimum designs except in the region of low flow rate.
机译:通过混合多目标进化算法(MOEA)与响应面近似(RSA)替代模型,提出了轴流通风机设计的优化程序。通过使用切应力传递(SST)湍流模型求解三维(3-D)雷诺平均Navier-Stokes(RANS)方程,进行了初步风扇设计的数值分析。多目标优化过程执行两次以了解不同变量的耦合效果。第一个多目标优化过程是通过三个设计变量定义轮毂,中跨和顶部的交错角进行的,第二个多目标优化过程是通过五个设计变量进行定义的轮毂对尖端的比率,轮毂盖安装距离,轮毂盖比率,以及中跨和尖端的交错角度。选择两个空气动力学性能参数,即总效率和总压力升高作为优化的目标函数。这些目标函数是通过3-D RANS分析在设计空间中通过拉丁超立方体采样所采样的设计点进行数值评估的。优化后,效率最高提高了1.8%,压力上升提高了31.4%。在大多数最佳设计中,除了低流速区域外,非设计性能也得到了改善。

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