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APS -70th Annual Meeting of the APS Division of Fluid Dynamics- Event - Direct numerical simulations of an arc-powered heater for used in a hypersonic wind tunnel

机译:APS-APS流体动力学分部第70届年会-事件-高超音速风洞中使用的电弧动力加热器的直接数值模拟

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We study a model arc-heater using direct numerical simulations, in a configuration motivated by its used to generated inflow of a high-speed wind tunnel for hypersonics research. The flow is assumed to be in local thermal equilibrium (LTE) and is modeled with with 11 species (N$_2$ , O$_2$, NO, N, O, N$^+_2$ , O$^+_2$ , NO$^+$, N$^+$, O$^+$, $e^-$). The flow equations are solved in conjunction with an electrostatic field solver and the gas electric conductivity in LTE. The flow rate and the mean arc power are set to be $50.42,$g/s and $84.7 ,$kW with $214.0,$V of the mean arc voltage , respectively. We study the flow details, the heading and thrust mechanisms, and make general comparisons with a corresponding, though geometrically more complex, experimental configuration. We particularly interested in the radical species it produces and will potentially be present in the wind-tunnel test section.
机译:我们使用直接数值模拟研究电弧加热器的模型,该模型在其构造的推动下用于产生超音速研究的高速风洞流入。假定流动处于局部热平衡(LTE)中,并用11种物质进行建模(N $ _2 $,O $ _2 $,NO,N,O,N $ ^ + _ 2 $,O $ ^ + _ 2 $ ,NO $ ^ + $,N $ ^ + $,O $ ^ + $,$ e ^-$)。结合静电场求解器和LTE中的气体电导率来求解流方程。流量和平均电弧功率分别设置为$ 50.42,$ g / s和$ 84.7,$ kW,其中平均电弧电压为$ 214.0,$ V。我们研究了流的细节,航向和推力机制,并与相应的,虽然几何上更复杂的实验配置进行了一般比较。我们对它产生的自由基种类特别感兴趣,并且可能会在风洞测试部分中出现。

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