| 杨志斌,成竹,任青梅,李喜明,蒋军亮.飞机结构三维温度场分析程序[J].计算力学学报,2004,21(4):498~501 |
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| 飞机结构三维温度场分析程序 |
| Three-dimensional temperature field analysis in aircraft structure |
| 修订日期：2002-10-16 |
| DOI：10.7511/jslx20044088 |
| 中文关键词: 温度场 有限元 接触热阻 |
| 英文关键词:temperature field,finite element,thermal contact resistance |
| 基金项目: |
| 杨志斌 成竹 任青梅 李喜明 蒋军亮 |
| 中国飞机强度研究所,西安710065 |
| 摘要点击次数: 1479 |
| 全文下载次数: 8 |
| 中文摘要: |
| 介绍了“飞机结构三维温度场分析”程序。该程序具有完整的自动建模体系和云图曲线显示功能。通过试验测定了“热阻”参数，进而在程序中增加了热阻元以处理不同结构件的接触问题，考虑了空气动力加热载荷情形。经过许多工程算例，结果良好。 |
| 英文摘要: |
| The program analysing aircraft structure three-dimensional temperature field is introduced in this paper. The program has an integrated automatic system to make patterns. And the displaying function is made by cloud chart. The coefficient of thermal resistance is defined, and the contact question of different structure pieces displaced by thermal resistance element is added in the program. Through studying heated load situation of air power. The calculation results show fine in many engineering calculations. |
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