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PREDICTION OF CONVECTIVE AND UV-VISIBLE RANGE RADIATIVE FLUXES FOR MARS ENTRY – CONTRIBUTION TO TEST CASE 3

机译:用于火星入学对流和UV可见范围辐射通量的对流和UV可见范围辐射通量 - 贡献测试案例3

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Recent work on the ESA Plasma Radiation Database (PARADE) on CO_2 flows and the addition of a collisional-radiative capability to the Navier-Stokes code TINA has enabled an assessment to be made of the excited states of CO and C_2 in the flowfield in the RHTG test case 3. Flowfield calculations have been performed for the frontshield only and the radiative fluxes in the UV-visible range from CO and C_2 have been calculated. The findings show flowfield and radiative flux results consistent with previous contributions, and a reduction in the radiation from the application of the collisional-radiative model.
机译:CO_2流量的ESA等离子数据库(PARACE)的最新工作以及向Navier-Stokes Code TINA的碰撞 - 辐射能力使得能够在流场中的CO和C_2的激发态进行评估 rhtg测试盒3.仅对FrontShield执行了Flowfield计算,并且已经计算了CO和C_2的UV可见范围内的辐射通量。 调查结果显示流动场和辐射助焊剂与以前的贡献一致,以及从碰撞辐射模型的应用中减少辐射。

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