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Spectral element/smoothed profile method for turbulent flow simulations of waterjet propulsion systems

机译:用于水射流推进系统湍流模拟的光谱元素/平滑轮廓法

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摘要

We have developed fast numerical algorithms [1] for flows with complex moving domains, e.g. propellers in free-space and impellers in waterjets, by combining the smoothed profile method (SPM, [2, 3, 4]) with the spectral element method [5]. The new approach exhibits high-order accuracy with respect to both temporal and spatial discretizations. Most importantly, the method yields great computational efficiency as it uses fixed simple Cartesian grids and hence it avoids body-conforming mesh and remeshing. To simulate high Reynolds number flows, we incorporate the Spalart-Allmaras turbulence model and solve the unsteady Reynolds-averaged Navier-Stokes (URANS) equations. We present verification of the method by studying the turbulent boundary layer over a flat plate. We show that both the eddy viscosity and velocity fields are resolved very accurately within the boundary layer. Having developed and validated our numerical approach, we apply it to study transitional and turbulent flows in an axial-flow waterjet propulsion system. The efficiency and robustness of our method enable parametric study of many cases which is required in design phase. We present performance analysis and show the agreement with experimental data for waterjets.
机译:我们已经针对具有复杂运动域的流(例如,水流)开发了快速的数值算法[1]。自由空间的螺旋桨和喷水器的叶轮,通过结合平滑轮廓法(SPM,[2,3,4])和谱元素法[5]。新方法在时间和空间离散方面都显示出高阶精度。最重要的是,由于该方法使用固定的简单笛卡尔网格,因此产生了很高的计算效率,因此避免了贴合人体的网格和重新网格化。为了模拟高雷诺数流,我们引入了Spalart-Allmaras湍流模型,并求解了不稳定的雷诺平均Navier-Stokes(URANS)方程。通过研究平板上的湍流边界层,我们提出了对该方法的验证。我们表明,涡流粘度场和速度场都在边界层内非常精确地解析了。在开发并验证了我们的数值方法之后,我们将其应用于研究轴流喷水推进系统中的过渡流和湍流。我们方法的效率和鲁棒性使设计阶段所需的许多情况可以进行参数研究。我们目前进行性能分析,并表明与水射流的实验数据一致。

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