4.7 Article

Mesh Properties for RANS Simulations of Airfoil-Shaped Profiles: A Case Study of Rudder Hydrodynamics

期刊

出版社

MDPI
DOI: 10.3390/jmse9101062

关键词

rudder hydrodynamics; mesh properties; mesh independence; computational fluid dynamics

资金

  1. National Natural Science Foundation of China [62003250]
  2. Research on Intelligent Ship Testing and Verification [2018473]
  3. Program of Marine Economy Development Special Fund (Six Marine Industries) under Department of Natural Resources of Guangdong Province [GDNRC[2021]59]

向作者/读者索取更多资源

This article presents a case study on ship rudders to investigate the impacts of different mesh properties on the accuracy of hydrodynamic coefficients obtained by CFD methods. Recommended mesh properties, including Reynolds numbers, domain sizes, and node distributions, are provided for airfoil-shaped profiles. The study clarifies the influences of mesh properties on rudder hydrodynamics and offers applicable settings for other airfoil-shaped profiles.
A good mesh is a prerequisite for achieving reliable results from Computational Fluid Dynamics (CFD) calculations. Mesh properties include mesh types, computational domain sizes, and node distributions. However, in literature, we found no clear consensus about what these properties should be. In this article, we performed a case study on ship rudders to determine what the suitable mesh properties are for airfoil-shaped profiles. A classic NACA 0012 profile is chosen as an example, and commercial packages ANSYS ICEM are applied for meshing with an ANSYS Fluent solver. With a strategy in consideration of relationships among different mesh properties, a comprehensive parametric investigation is conducted to study the impacts of these properties on the accuracy of rudder hydrodynamic coefficients obtained by CFD methods. The step-by-step study outputs recommended Reynolds numbers, domain sizes, and near- and far-field node distributions for mesh types with distinct topology structures, i.e., C-mesh, O-mesh, H-mesh, and Hybrid-mesh. Specifically, the study shows that a critical Reynolds number is needed for the perspective of efficiency, while a domain extending 60 times of the chord length enables the boundary effects to be negligible. As for node distributions, the near-field nodes should be treated carefully, compared with those in the far-field. After that, corresponding mesh properties for different calculation objectives are illustrated in detail based on the characteristics of mesh types mentioned above. With the proposed strategy for mesh refinements, impacts of different mesh properties on rudder hydrodynamics are clarified and recommended settings are applicable for other airfoil-shaped profiles such as wind turbines and marine propellers.

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