| 液体火箭发动机动态特性数学模型的验证 |
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| 引用本文： | 沈赤兵,吴建军,陈启智.液体火箭发动机动态特性数学模型的验证[J].推进技术,1998,19(6):1-6. |
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| 作者姓名： | 沈赤兵 吴建军 陈启智 |
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| 作者单位： | 国防科技大学航天技术系,长沙,410073 |
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| 摘 要： | 用试车数据检验某泵压液体火箭发动机动态特性非线性数学模型的准确度，考虑了发动机参数实际测量的误差范围。计算结果表明：在整个过渡过程中，所有可以实际测量的发动机参数的计算值与实测值之间的偏差均在±７．１％以内。
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| 关 键 词： | 液体推进剂火箭发动机，动态特性，数学模型，验证 |
| 修稿时间： | 1997-12-25 |
VERIFICATION OF MATHEMATICAL MODEL OF DYNAMIC CHARACTERISTICS FOR LIQUID ROCKET ENGINE |
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| Shen Chibing,Wu Jianjun and Chen Qizhi.VERIFICATION OF MATHEMATICAL MODEL OF DYNAMIC CHARACTERISTICS FOR LIQUID ROCKET ENGINE[J].Journal of Propulsion Technology,1998,19(6):1-6. |
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| Authors: | Shen Chibing Wu Jianjun and Chen Qizhi |
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| Institution: | Dept of Aerospace Technology,National Univ of Defence Technology,Changsha,410073;Dept of Aerospace Technology,National Univ of Defence Technology,Changsha,410073;Dept of Aerospace Technology,National Univ of Defence Technology,Changsha,410073 |
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| Abstract: | Test data are used to verify the nonlinear mathematical model of dynamic characteristics of a pump fed liquid rocket engine The actual measurement error range of engine parameters were considered during the model verification The results of the model verification show that the deviation between the actual measurement and calculation results based on the nonlinear model of engine parameters being able to be measured is in ±7 1% The deviation is in the allowable range of engineering use |
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| Keywords: | Liquid propellant rocket engine Dynamic characteristics Mathematical model Verification |
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