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A Novel Viscous Vortex Particle Method as Applied to Unsteady Rotor Wake Modeling and Simulation

机译:一种新的粘性涡旋粒子方法在非定常转子尾迹建模与仿真中的应用

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This paper summarizes the development and validation of a novel viscous vortex particle method (VVPM) as applied to the challenging unsteady rotor wake problem. The viscous vortex particle model developed is based on first principles and solves for the rotor wake vorticity convection and diffusion in the velocity-vorticity form of the incompressible Navier-Stokes equation. Compared to conventional rotor wake solutions, such as the free wake model, the VVPM can accurately address the rotor wake distortion, the tip vortex roll-up, and the vorticity diffusion from the first principle solution without relying on any empirical estimation of the modeling parameters as is required for existing free wake codes. The current grid based Navier-Stokes CFD methods also encounter the serious hurdle of artificial numerical dissipation due to the numerical discretization and, hence, cannot accurately capture the rotor wake vorticity variation for accurate rotor performance prediction or for any meaningful analysis of aerodynamic interactional problems. The VVPM developed through this research adopts a grid-free Lagrangian simulation where there is no artificial numerical dissipation involved. This paper discusses the theoretical viscous vortex particle formulation and the corresponding numerical technique for the rotor wake solution. The simulation results obtained agreed well with measured data, which validates the new viscous vortex particle method.
机译:本文总结了一种新颖的粘性涡旋粒子方法(VVPM)的开发和验证,该方法适用于具有挑战性的非定常转子尾流问题。所开发的粘性涡旋颗粒模型基于第一原理,并以不可压缩的Navier-Stokes方程的速度-涡旋形式解决了转子尾流的涡旋对流和扩散。与传统的转子尾流解决方案(例如自由尾流模型)相比,VVPM可以精确地解决转子尾流畸变,尖端涡旋累积以及来自第一个原理解的涡度扩散,而无需依赖任何对模型参数的经验估算现有的免费唤醒代码所要求的。由于数值离散,当前基于网格的Navier-Stokes CFD方法还遇到了严重的人工数值耗散障碍,因此无法准确捕获转子尾流涡度变化以进行准确的转子性能预测或任何有意义的气动相互作用问题分析。通过这项研究开发的VVPM采用了无网格拉格朗日模拟,其中没有人为的数值耗散。本文讨论了转子涡流解的理论粘性涡旋颗粒公式和相应的数值技术。仿真结果与实测数据吻合良好,验证了新的粘性涡旋粒子法。

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