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Research on the Simulation Method of External Ballistic Flight Speed of Fuze

机译:引信外弹道飞行速度的仿真方法研究

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To solve the problem of getting different blowing speed of turbine motor after assembling turbine motor blower of fuze, do the analysis of free jet theory, and deduce the axis velocity formula on the basis of predecessor' research results. According to the theory of fluid mechanics, do the free jet simulation experiment of the round nozzle of constant diameter in the air, and get the data of the axis velocity. Compare the chart between the simulation results and the theoretical formula, in the condition of a lot of difference, according to the presumption of form from the theory of jet velocity, with simulation data as sample, using MATLAB as the tool, fitting out of the axis velocity distribution formula, provide theory basis for testing the turbo air motor speed regulation the simulation results and the theoretical formula, in accord with degree of poor situation, according to the theory of jet velocity equations are the axis of the presumption of form, with simulation data as sample, using MATLAB as the tool, fitting out of the axis velocity distribution formula, for the adjusting the blowing speed of turbine motor in the test.
机译:为了解决涡轮机电动机涡轮机电动机的不同吹速度的问题,对引渡涡轮机电机鼓风机进行自由喷射理论进行分析,并在前任研究结果的基础上推断轴速度公式。根据流体力学理论,在空气中进行圆形喷嘴的自由喷射模拟实验,并获得轴速度的数据。比较仿真结果与理论公式之间的图表,在大量差异的情况下,根据喷射速度理论的推定,用模拟数据作为样品,使用MATLAB作为工具,拟合轴速度分配公式,为测试涡轮机气动电机调速提供理论依据,仿真结果和理论公式,根据换气速度等级的程度,根据喷射速度方程的理论是形式推定的轴线,与将数据作为样品,使用MATLAB作为工具,拟合出轴速度分布式公式,用于调节试验中涡轮电机的吹送速度。

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