Seunghyun Kim, S. Kinnas, Ray Thomas Grebstad, Jahn Terje Johannessen
{"title":"Hydrodynamic Analysis of a Triple Thruster Unit Via a BEM/RANS Interactive Method","authors":"Seunghyun Kim, S. Kinnas, Ray Thomas Grebstad, Jahn Terje Johannessen","doi":"10.1115/omae2022-81026","DOIUrl":null,"url":null,"abstract":"\n In this paper, a boundary element method (BEM) is used to predict the unsteady performance of ducted propellers in open water and ship behind conditions. The model propeller adopted includes the non-axisymmetric duct appendages (e.g., gearbox, brackets, and vertical structure connected to the hub), which induce severe shedding vortices on the propeller plane. This study thus investigates the effects of separation from the duct appendages as well as the upstream hull on the unsteady ducted propeller performance under different loading conditions. To improve the accuracy of a potential flow solver for highly viscous problems with separated flow near a blunt body, the present method is coupled with a viscous Reynolds-Averaged Navier-Stokes (RANS) solver. The former solves the ducted propeller problem to produce the propeller-induced flow field and body forces, with which the latter solves the total flow field based on a finite volume method. This approach is implemented in an iterative manner until the predicted 3D effective wake on the propeller surface becomes fully converged. An automated interface is developed to facilitate this process. A complete analysis of the propeller performance (i.e., predicted effective wake, flow-field, unsteady forces, and circulations on the blade) is presented at various operating conditions to investigate how the flow field inside and outside the nozzle is influenced by the viscous interaction among the incoming flow, propeller, its appendages, and upstream hull. For the sake of validation, the predicted results are compared with experimental measurements and results from unsteady full-blown RANS simulations. The presented results show satisfactory agreement among the results from different approaches, which makes the BEM/RANS coupling scheme adequate and computationally efficient for practical applications.","PeriodicalId":408227,"journal":{"name":"Volume 5A: Ocean Engineering","volume":"3 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-06-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Volume 5A: Ocean Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1115/omae2022-81026","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
In this paper, a boundary element method (BEM) is used to predict the unsteady performance of ducted propellers in open water and ship behind conditions. The model propeller adopted includes the non-axisymmetric duct appendages (e.g., gearbox, brackets, and vertical structure connected to the hub), which induce severe shedding vortices on the propeller plane. This study thus investigates the effects of separation from the duct appendages as well as the upstream hull on the unsteady ducted propeller performance under different loading conditions. To improve the accuracy of a potential flow solver for highly viscous problems with separated flow near a blunt body, the present method is coupled with a viscous Reynolds-Averaged Navier-Stokes (RANS) solver. The former solves the ducted propeller problem to produce the propeller-induced flow field and body forces, with which the latter solves the total flow field based on a finite volume method. This approach is implemented in an iterative manner until the predicted 3D effective wake on the propeller surface becomes fully converged. An automated interface is developed to facilitate this process. A complete analysis of the propeller performance (i.e., predicted effective wake, flow-field, unsteady forces, and circulations on the blade) is presented at various operating conditions to investigate how the flow field inside and outside the nozzle is influenced by the viscous interaction among the incoming flow, propeller, its appendages, and upstream hull. For the sake of validation, the predicted results are compared with experimental measurements and results from unsteady full-blown RANS simulations. The presented results show satisfactory agreement among the results from different approaches, which makes the BEM/RANS coupling scheme adequate and computationally efficient for practical applications.
本文采用边界元法(BEM)对导管式螺旋桨在开阔水域和船后工况下的非定常性能进行了预测。所采用的模型螺旋桨包括非轴对称风道附件(如齿轮箱、托架、与轮毂连接的垂直结构),这些附件在螺旋桨平面上产生严重的脱落涡。因此,本文研究了不同载荷条件下,与管道附属物分离以及上游船体分离对非定常导管螺旋桨性能的影响。为了提高钝体附近具有分离流的高粘性问题的势流求解器的精度,将该方法与粘性reynolds - average Navier-Stokes (RANS)求解器相结合。前者解决了导管式螺旋桨问题,产生了螺旋桨诱导的流场和体力,后者基于有限体积法求解了总流场。该方法以迭代的方式实现,直到预测的螺旋桨表面三维有效尾迹完全收敛。开发了一个自动化界面来促进这一过程。对不同工况下的螺旋桨性能(即预测的有效尾迹、流场、非定常力和叶片上的循环)进行了完整的分析,以研究来流、螺旋桨及其附属物和上游船体之间的粘性相互作用对喷管内外流场的影响。为了验证预测结果,将预测结果与实验测量结果和非定常全面RANS模拟结果进行了比较。结果表明,不同方法的计算结果具有较好的一致性,表明BEM/RANS耦合方案具有较好的计算效率。