| 航天飞机防热结构温度场的数值计算研究 |
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| 引用本文： | 耿为群,黄振中.航天飞机防热结构温度场的数值计算研究[J].空气动力学学报,1992,10(3):367-372. |
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| 作者姓名： | 耿为群 黄振中 |
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| 作者单位： | 中国空气动力研究与发展中心，中国空气动力研究与发展中心，国家科委信息研究所 四川绵阳 621000，四川绵阳 621000，北京 100862 |
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| 摘 要： | 本文采用有限差分法及有限元素法计算了航天飞机防热结构的一、二维温度分布,并与飞行实测数据及实验结果进行了比较,符合较好。
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| 关 键 词： | 航天飞机 热防护系统 数值计算 |
Numerical Analysis of the Transient Temperature Field of the Multilayer Insulative Systems of Space Shuttle |
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| Geng Weiqun Yang Maozhao.Numerical Analysis of the Transient Temperature Field of the Multilayer Insulative Systems of Space Shuttle[J].Acta Aerodynamica Sinica,1992,10(3):367-372. |
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| Authors: | Geng Weiqun Yang Maozhao |
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| Institution: | Geng Weiqun Yang Maozhao(China Aerodynamics Research and Development Center)Huang Zhenzhong (Beijing Information Institute) |
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| Abstract: | In the paper the finite difference method and the finite element method have been used to determine the temperature distribution through the multilayer isulative systems of the space shuttle. The computed results have been compared with the STS-2 flight data and other experimental results; they show good agreements. |
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| Keywords: | space shuttle TPS numerical method heat-conduction equation |
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