论文标题

在球体上流动的一般阻力系数

A General Drag Coefficient for Flow over a Sphere

论文作者

Singh, Narendra, Kroells, Michael, Li, Chenxi, Ching, Eric, Ihme, Matthias, Hogan, Christopher J., Schwartzentruber, Thomas

论文摘要

得出了在流体中移动的球形颗粒的阻力系数的总体物理表达。所提出的相关性结合了必需的稀有物理,低速流体动力学和冲击波物理学,以准确地对粒子可能会经历的各种Mach和Knudsen数字(因此雷诺数)进行准确模拟颗粒拖拉力。由于基于物理的缩放定律的衍生基础,该提出的相关性嵌入了气体特异性的特性,并且明确依赖于在恒定压力和恒定体积下特定热能的比率。该相关性适用于任意粒子相对速度,颗粒直径,气压,气温和表面温度。与现有的阻力模型相比,相关性显示为更准确地重现了广泛的实验数据。最后,将新的相关性应用于模拟高速流中尘埃颗粒的轨迹,这与进入火星大气的航天器有关。发现由于颗粒冲击而引起的增强的表面热通量对粒子阻力模型很敏感。

A generalized physics-based expression for the drag coefficient of spherical particles moving in a fluid is derived. The proposed correlation incorporates essential rarefied physics, low-speed hydrodynamics, and shock-wave physics to accurately model the particle-drag force for a wide range of Mach and Knudsen numbers (and therefore Reynolds number) a particle may experience. Owing to the basis of the derivation in physics-based scaling laws, the proposed correlation embeds gas-specific properties and has explicit dependence on the ratio of specific heat capacities at constant pressure and constant volume. The correlation is applicable for arbitrary particle relative velocity, particle diameter, gas pressure, gas temperature, and surface temperature. Compared to existing drag models, the correlation is shown to more accurately reproduce a wide range of experimental data. Finally, the new correlation is applied to simulate dust particles' trajectories in high-speed flow, relevant to a spacecraft entering the Martian atmosphere. The enhanced surface heat flux due to particle impact is found to be sensitive to the particle drag model.

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