Design of High Altitude Propeller Using Multilevel Optimization
作者: Xinqiang LiuWeiliang HeFengmei Wei
刊名: International Journal of Computational Methods, 2020, Vol.17 (04), pp.32
来源数据库: World Scientific Publishing
DOI: 10.1142/S021987621950004X
关键词: High altitude propellerMultilevel optimizationBlade element momentum theoryMIGANSGA-IICFD simulation
原始语种摘要: An improved D’Angelo optimization framework based on the surrogate model and optimization algorithm is proposed to design and optimize a new high altitude propeller which is applied to the propulsion system of the stratospheric aircraft. The framework adopts a multilevel optimization strategy to determine a high efficiency and light weight propeller. The aerodynamic characteristics of S1223 airfoil are calculated by Computational Fluid Dynamics (CFD) method. The aerodynamic performance of the D’Angelo propeller which is obtained by the first-level optimization is predicted by Blade element momentum (BEM) theory. Then the D’Angelo propeller chord and twist angle, which are regarded as the initial conditions of the second-level optimization, are optimized to achieve the maximum efficiency...
全文获取路径: World Scientific Publishing  (合作)
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关键词翻译
关键词翻译
  • propeller 螺旋桨
  • optimization 最佳化
  • aerodynamic 气体动力的
  • momentum 动量
  • efficiency 效率
  • level 水准
  • framework 构架
  • minimize 最小化
  • agreement 协议
  • genetic 遗传的