| 某导弹弹体对主发动机转子振动的响应 |
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| 引用本文： | 徐学文,徐新琦,袁书生. 某导弹弹体对主发动机转子振动的响应[J]. 振动与冲击, 2003, 22(3): 86-88 |
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| 作者姓名： | 徐学文 徐新琦 袁书生 |
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| 作者单位： | 海军航空工程学院,机械工程系,烟台,264001 |
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| 摘 要： | 根据主发动机在转子最大不平衡量作用下产生的激振力，应用动态分析有限元法计算了导弹飞行过程中弹体在发动机额定转速和巡航转速下的稳态响应，为进一步分析弹上仪器的响应及其可靠性提供理论依据。
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| 关 键 词： | 导弹 弹体 主发动机转子 振动 响应 不平衡量 激振力 可靠性 |
| 修稿时间： | 2002-07-10 |
Response of Guided Missile Body to Vibration of Main Engine Rotor |
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| Xu Xuewen Xu Xinqi Yuan Shusheng. Response of Guided Missile Body to Vibration of Main Engine Rotor[J]. Journal of Vibration and Shock, 2003, 22(3): 86-88 |
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| Authors: | Xu Xuewen Xu Xinqi Yuan Shusheng |
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| Abstract: | According to the excitations generated by main engine under the largest imbalance of the rotor,the stable response of missile body is calculated at the specified speed and cruising speed of engine during the flying of guided missile using finite element method in dynamic analysis.The response data at some locations missile body are given in order to further analyze the responses and reliabilities of the instruments in missile. |
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| Keywords: | guided missile finite element method response vibration |
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