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本文用Nocilla粒子-表面作用模型计算卫星在运行轨道中整体气动力系数和星体表面热流密度分布,文中列出了详细计算公式和一个算例。
In this paper, the Nocilla particle-surface interaction model is used to calculate the global aerodynamic coefficients of the satellite in the orbit and the surface heat flux density distribution. A detailed calculation formula and an example are given in this paper.