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Internal ballistics simulation based on object oriented programming

机译:基于面向对象程序设计的内部弹道仿真

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The knowledge of internal ballistics simulation is quite obscure due to security reason related to rocket implementation for national defense. Internal ballistics simulation involves complex calculation of thrust profile generated by burning solid propellant mass. The design of appropriate solid propellant mass for desired thrust profile requires visualization of propellant mass and overlook how it burns from the start to the end. Object-oriented programming has been used as a tool for simulation of complex mathematic algorithms in many fields. This paper introduced object-oriented programming framework and software architecture for solving complex calculation of thrust profile and visualization of burning solid propellant. JAVA programming language is chosen to implement a test program for proving objected-oriented programming based internal ballistics simulation. The result shows the reasonable trend of thrust profile according to the real behavior of thrust generated by solid propellant. This paper gives intuitive idea of implementing simulation tool for designing of solid propellant mass in rocket application.
机译:由于与用于国防的火箭实施相关的安全原因,内部弹道模拟的知识非常模糊。内部弹道仿真涉及燃烧固体推进剂物质产生的推力剖面的复杂计算。为实现所需的推力曲线而设计合适的固体推进剂质量,需要对推进剂质量进行可视化,并忽略其从头到尾的燃烧方式。面向对象编程已在许多领域中用作模拟复杂数学算法的工具。本文介绍了面向对象的编程框架和软件体系结构,用于解决推力剖面的复杂计算和燃烧固体推进剂的可视化。选择JAVA编程语言来实现测试程序,以证明基于面向对象的程序的内部弹道仿真。结果表明,根据固体推进剂产生的推力的真实行为,推力曲线具有合理的趋势。本文给出了在火箭应用中实现用于设计固体推进剂质量的仿真工具的直观思路。

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