A surrogate-model-based aerodynamic optimization design method for cycloidal propeller in hover was proposed,in order to improve its aerodynamic efficiency,and analyze the basic criteria for its aerodynamic optimizati...A surrogate-model-based aerodynamic optimization design method for cycloidal propeller in hover was proposed,in order to improve its aerodynamic efficiency,and analyze the basic criteria for its aerodynamic optimization design.The reliability and applicability of overset mesh method were verified.An optimization method based on Kriging surrogate model was proposed to optimize the geometric parameters for cycloidal propeller in hover with the use of genetic algorithm.The optimization results showed that the thrust coefficient was increased by 3.56%,the torque coefficient reduced by 12.05%,and the figure of merit(FM)increased by 19.93%.The optimization results verified the feasibility of this design idea.Although the optimization was only carried out at a single rotation speed,the aerodynamic efficiency was also significantly improved over a wide range of rotation speeds.The optimal configuration characteristics for micro and small-sized cycloidal propeller were:solidity of 0.2-0.22,maximum pitch angle of 25°-35°,pitch axis locating at 35%-45% of the blade chord length.展开更多
摆线推进器在旋转过程中,叶片的迎流角实时变化以产生推力。文章将使用FLUENT软件,研究摆线推进器在不同工作参数下的水动力性能。根据摆线推进器的运动规律,编写相应的用户自定义函数(User Defined Function,UDF)控制叶片做摆线运动。...摆线推进器在旋转过程中,叶片的迎流角实时变化以产生推力。文章将使用FLUENT软件,研究摆线推进器在不同工作参数下的水动力性能。根据摆线推进器的运动规律,编写相应的用户自定义函数(User Defined Function,UDF)控制叶片做摆线运动。在仿真中使用非结构网格、滑移网格方法来分析推进器叶片在不同转轴比、进速系数、转速以及偏心点时对摆线推进器水动力性能的影响。研究结果表明,在50%左右的转轴比、中高进速、较低转速以及小偏心点时,推进器的水动力参数波动较小,有助于维持推力以及叶片稳定性。展开更多
文摘A surrogate-model-based aerodynamic optimization design method for cycloidal propeller in hover was proposed,in order to improve its aerodynamic efficiency,and analyze the basic criteria for its aerodynamic optimization design.The reliability and applicability of overset mesh method were verified.An optimization method based on Kriging surrogate model was proposed to optimize the geometric parameters for cycloidal propeller in hover with the use of genetic algorithm.The optimization results showed that the thrust coefficient was increased by 3.56%,the torque coefficient reduced by 12.05%,and the figure of merit(FM)increased by 19.93%.The optimization results verified the feasibility of this design idea.Although the optimization was only carried out at a single rotation speed,the aerodynamic efficiency was also significantly improved over a wide range of rotation speeds.The optimal configuration characteristics for micro and small-sized cycloidal propeller were:solidity of 0.2-0.22,maximum pitch angle of 25°-35°,pitch axis locating at 35%-45% of the blade chord length.
文摘摆线推进器在旋转过程中,叶片的迎流角实时变化以产生推力。文章将使用FLUENT软件,研究摆线推进器在不同工作参数下的水动力性能。根据摆线推进器的运动规律,编写相应的用户自定义函数(User Defined Function,UDF)控制叶片做摆线运动。在仿真中使用非结构网格、滑移网格方法来分析推进器叶片在不同转轴比、进速系数、转速以及偏心点时对摆线推进器水动力性能的影响。研究结果表明,在50%左右的转轴比、中高进速、较低转速以及小偏心点时,推进器的水动力参数波动较小,有助于维持推力以及叶片稳定性。
