| 固体火箭发动机固有频率灵敏度特性的初步研究 |
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| 引用本文： | 谭三五,钟莉.固体火箭发动机固有频率灵敏度特性的初步研究[J].推进技术,1991,12(5):16-20. |
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| 作者姓名： | 谭三五 钟莉 |
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| 作者单位： | 航空航天部41所
(谭三五)，西安交通大学(钟莉) |
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| 摘 要： | 本文运用固有频率灵敏度分析方法,把长细比较大发动机简化为梁模型,推导出其固有频率灵敏度计算公式;对于长细比较小发动机必需采用有限元模型,本文采用简化方法,进行固有频率灵敏度分析,并归纳出两种发动机的灵敏度特性.
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| 关 键 词： | 固体推进剂 火箭发动机 结构振动 结构动力学 |
PRELIMINARY INVESTIGATION OF THE CHARACTERISTICS OF SENSITIVITY OF FREQUENCY IN A SOLID ROCKET MOTOR |
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| Tan Sanwu and Zhong Li.PRELIMINARY INVESTIGATION OF THE CHARACTERISTICS OF SENSITIVITY OF FREQUENCY IN A SOLID ROCKET MOTOR[J].Journal of Propulsion Technology,1991,12(5):16-20. |
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| Authors: | Tan Sanwu and Zhong Li |
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| Institution: | Tan Sanwu Zhong Li
(The 41st Research Institute) (Xi'an Jiaotong University) |
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| Abstract: | A analytical method of sensitivity of frequency is used to obtain the formula of sensitivity for high length-diameter ratio solid rocket motor by using beam model. Sensitivity for low length-diameter ratio motor is analyzed by using finite element model with simplified method,Some sensitivity characteristics of these two type of motors are obtained,e.g,the various order sensitivities of frequency is in constant ratio for the beam model, and ind-ependant of structural parameters of motor. |
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| Keywords: | Solid rocket engine Structural vibration Structural dynamics |
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