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External Aerodynamic Study on Wing in Ground Effect (Wig) Marine Vehicle Using Computational Fluid Dynamics (Cfd)

机译:使用计算流体动力学(CFD)地面效果(WIG)海洋车辆的外部空气动力学研究

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The study of the characteristics performances of a wing in ground effect marine vehicle iscarried out in this project; a computational fluid dynamics (CFD) method is employed through numericalsimulation to study the behavior of the fluid flow around the 3D WIG craft CAD model. The Navier StokesEquation, which is based on the Reynolds transport theory, and the K- omega SST turbulence model is solvedfor the aerodynamic flow around the wing in ground effect (WIG) 3D geometric CAD model. The hex-dominantmesh algorithm was used to discretize a largely enough computational domain to solve for convergence in thenumerical simulation, with the goal to obtain coherent and valid simulation run result.
机译:在这个项目中造成地面效果海洋车辆的翼特性的研究;通过数值刺激采用计算流体动力学(CFD)方法,以研究3D假发Craft CAD模型周围的流体流动的行为。基于雷诺运输理论的Navier Stokeequation,以及K-Omega SST湍流模型对机翼围绕地面效果(WIG)3D几何CAD模型的空气动力学流动求出。 Hex-DominantMesh算法用于离散一个很大程度上足够的计算域来解决overConical仿真中的收敛,目标是获得连贯和有效的模拟运行结果。

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