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Theoretical calculation of mid-infrared spectra from hypersonic non-ablative sphere

机译:高超声速非烧蚀球的中红外光谱的理论计算

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Hypersonic body moving in the atmosphere will suffer high temperature reacting flows which will emit complex radiation. Theoretical calculation was taken in this paper for a hypersonic non-ablative sphere. Hypersonic flow around the sphere was simulated using 9 species chemical kinetic and two temperature thermal non-equilibrium model. Based on this simulated flow field, the LOS method is used to solve radiative transfer and line-by-line model is used to calculate the spectrum from molecular and atoms in mid-infrared. The spectra from different components have been analyzed one by one. The calculation founds out that atom N and O diatomic molecule NO and bremsstrahlung will be important radiation source in this pure air hypersonic flow field. The radiation from hypersonic flow field has been analyzed in both high pressure environment and low pressure environment.
机译:在大气中运动的高超音速身体将遭受高温反应流,这将发出复杂的辐射。本文对高超声速非烧蚀球体进行了理论计算。使用9种化学动力学和两个温度热非平衡模型模拟了围绕球体的高超声速流动。在此模拟流场的基础上,使用LOS方法求解辐射传递,并使用逐行模型从中红外中的分子和原子计算光谱。来自不同成分的光谱已被一一分析。计算发现,在这种纯空气高超声速流场中,原子N和O的双原子分子NO和致辐射将是重要的辐射源。高声速流场的辐射已经在高压环境和低压环境中进行了分析。

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