{"title":"Application of a Comprehensive Design Method to Counter-Rotating Propellers","authors":"K. Cha, S. Kinnas","doi":"10.5957/tos-2022-003","DOIUrl":null,"url":null,"abstract":"A comprehensive design method is applied to design of counter-rotating propellers (CRP). A numerical nonlinear optimization algorithm is first used for design of each propeller. This approach represents a blade by B-spline geometry and the design variables at the location of the vertices of the B-spline polygon determine the optimal blade shape. The nonlinear optimization method aims at minimizing the torque for a given target thrust with constraints, e.g. the minimum pressure constraint for a fully wetted propeller or maximum allowed cavity area for a cavitating propeller. Then the interaction of the designed propellers and a given pod including the viscous flow field around the two propellers is analyzed by coupling a vortex-lattice method (VLM) with a Reynolds-Averaged Navier-Stokes (RANS) solver. The analysis determines a new inflow for a new design of propellers. The procedure of the design and interaction analysis finishes when the propeller thrust converges within a certain tolerance. Finally, the designed propellers are compared with the original propellers.","PeriodicalId":108360,"journal":{"name":"Day 1 Tue, February 22, 2022","volume":"9 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-02-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Day 1 Tue, February 22, 2022","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.5957/tos-2022-003","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
Abstract
A comprehensive design method is applied to design of counter-rotating propellers (CRP). A numerical nonlinear optimization algorithm is first used for design of each propeller. This approach represents a blade by B-spline geometry and the design variables at the location of the vertices of the B-spline polygon determine the optimal blade shape. The nonlinear optimization method aims at minimizing the torque for a given target thrust with constraints, e.g. the minimum pressure constraint for a fully wetted propeller or maximum allowed cavity area for a cavitating propeller. Then the interaction of the designed propellers and a given pod including the viscous flow field around the two propellers is analyzed by coupling a vortex-lattice method (VLM) with a Reynolds-Averaged Navier-Stokes (RANS) solver. The analysis determines a new inflow for a new design of propellers. The procedure of the design and interaction analysis finishes when the propeller thrust converges within a certain tolerance. Finally, the designed propellers are compared with the original propellers.
将综合设计方法应用于对旋螺旋桨的设计。首先采用数值非线性优化算法对各螺旋桨进行设计。该方法通过b样条几何形状表示叶片,b样条多边形顶点位置的设计变量确定最佳叶片形状。非线性优化方法的目的是在给定目标推力的约束下使扭矩最小,例如,对全湿螺旋桨的最小压力约束或对空化螺旋桨的最大允许空腔面积约束。然后,通过涡流点阵法(VLM)和reynolds - average Navier-Stokes (RANS)求解器耦合分析了所设计的螺旋桨与给定吊舱的相互作用,包括两个螺旋桨周围的粘性流场。分析确定了一种新的螺旋桨设计的新进流。当螺旋桨推力收敛到一定的容差范围内时,完成设计和相互作用分析。最后,将设计的螺旋桨与原螺旋桨进行了比较。