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碟形锥柱型药柱的燃烧规律

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装药设计方法影响发动机内弹道性能,为提高装药利用率,分别采用UG NX和MATLAB软件进行了建模和编程计算,得到了药柱燃烧过程中燃烧面积推移规律和残药率与设计参数的函数关系图,进行了算例分析.计算结果表明:以药柱外径D为基准,当环向槽圆弧半径r∈(0,0.05D),圆柱段内孔半径R2∈(0.1D,0.4D),环向槽圆弧圆心旋转半径R3∈(R2,0.42D),圆柱段长L2∈(0.4D,1.53D)时,药柱燃烧呈现先增面性后减面性.残药率与r和R2的变化趋势同为单调递减,残药率与L2∈的变化趋势为单调递增,残药率与R3的变化趋势为先增大后减小.从减轻质量,提高强度和提高产品加工制造的工艺性等方面综合考虑,建议优先选择碟形封头.计算结果与实际数据的最大相对误差为0.078%.
Combustion laws of dished head conic-column grain
Charge design methods affect the ballistic performance of the engine.In order to improve the charge utilization rate,UG NX and MATLAB software were used for modeling and programming of the calculation,and the function relationship diagram of the combustion surface,the residual drug rate and the design parameters during the combustion process of the drug column was obtained,and finally the example analysis was carried out.The results showed that when D was defined as the outer diameter of grain,and the relative radius of circular groove r was(0,0.05D),the relative radius of the hole in the cylindrical section R2 was(0.1D,0.4D),the relative radius of the circular center of the circular groove R3 was(R2,0.42D)and the length of the cylinder L2 was(0.4D,1.53D),the combustion law was progressive at first and then regressive.The waste grain rate and the change trend of r and R2 monotonically decreased,the waste grain rate and the change trend of L2 monotonically increased,and the waste grain rate and the change trend of R3 first increased and then decreased.From the aspects of weight reduction,improvement of the strength,processing and manufacturing,it is recommended to give priority to the dished head.The maximum relative error between the calculated result and the actual data was 0.078%.

dished head conic-column grainwaste grain rateburninglawsolid rocket motorwall thickness

杨艳羽、徐铭泽、费月、孙晓霞、黄金红、张以亭、高艳军、万峻成

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辽宁北方华丰特种化工有限公司,辽宁抚顺 113003

碟形锥柱型药柱 残药率 燃烧规律 固体火箭发动机 壁厚

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(1)
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