| 用Nocilla模型计算卫星气动力系数和热流密度分布 |
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| 引用本文： | 王仲莲.用Nocilla模型计算卫星气动力系数和热流密度分布[J].中国空间科学技术,1987,7(4):11. |
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| 作者姓名： | 王仲莲 |
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| 作者单位： | 空间飞行器总体设计部 |
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| 摘 要： | 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。
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| 关 键 词： | 气动力系数 热流 密度分布 计算 卫星 |
THE COMPUTATIONS OF AERODYNAMIC COEFFICIENTS AND HEAT TRANSFER RATE FOR SATELLITES BY THE NOCILLA MODE |
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| Wang Zhonglian.THE COMPUTATIONS OF AERODYNAMIC COEFFICIENTS AND HEAT TRANSFER RATE FOR SATELLITES BY THE NOCILLA MODE[J].Chinese Space Science and Technology,1987,7(4):11. |
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| Authors: | Wang Zhonglian |
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| Institution: | Beijing Institute of Spacecraft System Engineering |
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| Abstract: | In this paper the total aerodynamic coefficients and heat transfer rate over the satellites in orbit are calculated by the Nocilla particle-surface interaction mode and the detail calculating formula and one example are given. |
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| Keywords: | Aerodynamic coefficient Heat flow Deusity distribution Computation Satellite |
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