| 固体发动机网状点火器的数值计算及性能分析 |
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| 引用本文： | 张为华,贺军科.固体发动机网状点火器的数值计算及性能分析[J].固体火箭技术,1992(1):7-11. |
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| 作者姓名： | 张为华 贺军科 |
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| 作者单位： | 国防科技大学，国防科技大学 湖南长沙 410073，湖南长沙 410073 |
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| 摘 要： | 采用一维非定常流动模型和差分格式对网状点火器进行了数值计算,得到了它的性能数据,对实际工程设计具有一定的参考价值。
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| 关 键 词： | 固体火箭 火箭发动机 点火器 |
NUMERICAL CALCULATION AND PERFORMANCE ANALYSIS OF THE NET-LIKE IGNITOR OF A SOLID ROCKET MOTOR |
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| Zhang Weihua,He Junke National University of Defense Technology,Changsha,Hunan.NUMERICAL CALCULATION AND PERFORMANCE ANALYSIS OF THE NET-LIKE IGNITOR OF A SOLID ROCKET MOTOR[J].Journal of Solid Rocket Technology,1992(1):7-11. |
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| Authors: | Zhang Weihua He Junke National University of Defense Technology Changsha Hunan |
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| Institution: | Zhang Weihua,He Junke National University of Defense Technology,Changsha,Hunan,410073 |
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| Abstract: | A one-dimensional nonsteady-state flow model and a difference schemeare used for the numerical calculation of the net-like ignitor. Its performance data areobtained, which have a certain reference value for the actual engineering design. |
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| Keywords: | Solid rocket engine Rocket ignitor Performance analysis Calculation method |
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