| 某火箭发动机系统振动特性测试和仿真分析 |
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| 引用本文： | 董寻虎,张晓漫.某火箭发动机系统振动特性测试和仿真分析[J].火箭推进,2006,32(1):54-58. |
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| 作者姓名： | 董寻虎 张晓漫 |
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| 作者单位： | 1. 上海宇航系统工程研究所,上海,201108
2. 上海卫星工程研究所,上海,200240 |
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| 摘 要： | 从计算和试验两方面分别研究了某火箭一级发动机的振动特性。侧重介绍了模态试验和商业有限元软件在发动机振动特性快速分析中的具体应用,以及发动机三维有限元模型如何应用于全箭有限元梁模型。计算结果和试验结果吻合较好。
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| 关 键 词： | 发动机 有限元分析 模态试验 |
| 文章编号： | (2006)01-0054-05 |
| 收稿时间： | 2005-05-19 |
| 修稿时间： | 2005-11-09 |
Dynamics test and simulation of a launch vehicle engine system |
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| Dong Xunhu,Zhang Xiaoman.Dynamics test and simulation of a launch vehicle engine system[J].Journal of Rocket Propulsion,2006,32(1):54-58. |
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| Authors: | Dong Xunhu Zhang Xiaoman |
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| Institution: | 1.Shanghai Aerospace System Engineering Institute, Shanghai 201108, China; 2.Shanghai Satellite Engineedng Institute, Shanghai 200240, China |
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| Abstract: | The vibration characteristics of a first stage rocket engine were studied by simulation and test. The modal test and application of business FEM software in the fast dynamic analysis was introduced in detail. In the end the 3D Engine FEM mode was reduced to simple beam mode and the total rocket beam model was established. The result of simulation consisted with the modal test result very well. |
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| Keywords: | engine FEM analysis modal test |
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