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Unsteady analysis of the six DOF motion of a buoyantly rising submarine

机译:浮升潜艇的六个自由度运动的非定常分析

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The roll instability observed in buoyantly rising small to medium sized submarines is analyzed in this work using a computational fluid dynamics (CFD) RANS solver coupled to the six degree of freedom (DOF) solid body equations of motion for the submarine. The theoretical framework and the numerical implementation, in particular the fluid-rigid-body interaction methodology, are outlined in detail in conjunction with models for control, propulsion, and ballast blowing. The submarine-specific models are conventional while the RANS flow field predictions are compared with a coefficient-based model and validated against steady state wind tunnel data spanning the onset flow conditions of interest. Detailed analyses of full-scale rising stability scenarios identify the magnitude and onset behavior of contributing moments to the instability. The rolling moment generated by the sail was found to be the primary cause of the instability. Simulation results confirm the finding from a previous study that the emergence roll angle of the submarine is very sensitive to the initial heel (roll) angle. When the initial heel angle is a fraction of a degree, the emergence roll angle is too small to be of concern but an initial heel angle of 2° results in a significant emergence roll angle of 10°. Unsteady viscous effects due to vorticity trailing from the sail were observed but they were found to have an insignificant impact on roll instability for the scenarios investigated.
机译:在这项工作中,使用计算流体力学(CFD)RANS求解器与潜艇的六自由度(DOF)固体运动方程式相结合,分析了在中小型浮力上升中观察到的侧倾不稳定性。结合控制,推进和压载吹气模型,详细概述了理论框架和数值实现方法,特别是流体-刚体相互作用方法。潜艇特定模型是常规模型,而RANS流场预测与基于系数的模型进行比较,并针对跨越感兴趣的起始流动条件的稳态风洞数据进行了验证。对全面上升的稳定情景进行的详细分析确定了导致不稳定的力矩的大小和起伏行为。发现风帆产生的侧倾力矩是造成不稳定的主要原因。仿真结果证实了先前研究的发现,即潜艇的出射侧倾角对初始后跟(侧倾)角非常敏感。当初始横倾角为一度的几分之一时,出射侧倾角太小而不必担心,但是初始横倾角为2°会导致明显的10°出射横倾角。观察到由于风帆从船尾拖曳而产生的不稳定粘滞效应,但在所研究的情况下,它们对侧倾失稳的影响很小。

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