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Numerical investigation of supercritical methane in helically coiled tube on regenerative cooling of liquid rocket electromechanical actuator

机译:螺旋卷管螺旋卷管超临界甲烷对液体火箭机电致动器再生冷却的数值研究

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摘要

A numerical model employing the SST k-co turbulent model is built to predict the turbulent flow and heat transfer of supercritical methane in helically coiled tube for the heat dissipation of high-power electromechanical actuator. The heat transfer mechanism and the crucial influence factors viz. pressure and heat flux are discussed, and the comparison between the semi-empirical heat transfer correlations and the simulation results are performed. The calculation results indicate that (1) before the pseudo-critical point of supercritical methane in helically tube, the effect of the buoyancy caused by the thermophysical properties cannot be neglected; (2) the domination of the centrifugal force on the heat transfer after the pseudo-critical point of supercritical methane can be confirmed obviously, contributed to the non-uniform distribution of flow and heat transfer coefficient in cross sections; (3) pressure and heat flux both exhibit significant effects on heat transfer of supercritical methane in helically coiled tube; (4) the semi-empirical heat transfer correlation from Zhang a al. shows the best agreement against the simulation result in the present paper.
机译:采用SST k-CO湍流模型的数值模型是为了预测螺旋盘管中超临界甲烷的湍流和传热,用于高功率机电致动器的散热。传热机制及其关键影响因素。讨论了压力和热通量,并且进行了半经验传热相关性和模拟结果之间的比较。计算结果表明(1)在螺旋管中超临界甲烷的伪临界点之前,不能忽略由热物理性质引起的浮力的效果; (2)在超临界甲烷的伪临界点的伪临界点可以明显地确认离心力对离心力的影响,有助于横截面中的流动和传热系数的不均匀分布; (3)压力和热通量两者都对螺旋盘管的超临界甲烷的热传递显着影响; (4)Zhang A Al的半经验传热相关性。显示本纸张仿真结果的最佳协议。

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