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

机译:火星进入的对流和紫外可见辐射通量的预测-对测试案例3的贡献

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Recent work on the ESA Plasma Radiation Database(PARADE) on CO_2 flows and the addition of acollisional-radiative capability to the Navier-Stokescode TINA has enabled an assessment to be made of theexcited states of CO and C_2 in the flowfield in theRHTG test case 3. Flowfield calculations have beenperformed for the frontshield only and the radiativefluxes in the UV-visible range from CO and C_2 havebeen calculated. The findings show flowfield andradiative flux results consistent with previouscontributions, and a reduction in the radiation from theapplication of the collisional-radiative model.
机译:ESA等离子体辐射数据库的最新工作 (PARADE)上的CO_2流量,并添加一个 Navier-Stokes的碰撞辐射能力 代码TINA允许对以下内容进行评估: CO和C_2在流场中的激发态。 RHTG测试案例3。 仅针对前挡板和辐射 CO和C_2在紫外线可见范围内的通量为 已计算。研究结果显示流场和 辐射通量结果与以前的结果一致 贡献,并减少来自 碰撞辐射模型的应用。

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