Investigation of Wake Breakdown in Hover Using The HMB3 Solver

T. Fitzgibbon, Rinaldo Steininger, G. Barakos
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引用次数: 1

Abstract

The present study forms an investigation of wake breakdown in hover using the HMB3 solver. Simulations are performed for the PSP rotor blade in hover on a grid aimed at resolving the detailed flow structures in the rotor wake. An assessment of different solver settings is performed including time discretisation, spatial discretisation accuracy and turbulence modelling on the rotor wake resolution and formation of instabilities. A particular focus is put on the existence and resolution of S-shaped structures due to the interactions of the blade tip vortices with the shear layers.
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用HMB3求解器研究悬停尾迹击穿问题
本研究采用HMB3求解器对悬停尾迹击穿进行了研究。为了求解旋翼尾迹的详细流动结构,在网格上对旋翼叶片悬停状态进行了数值模拟。对不同的求解器设置进行了评估,包括时间离散化、空间离散化精度和旋翼尾迹分辨率和不稳定性形成的湍流建模。特别关注了由于叶尖涡与剪切层的相互作用而产生的s形结构的存在和分解。
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