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复合固体推进剂燃烧性能模拟计算的神经网络方法
引用本文:邓鹏图,田德余,庄逢辰.复合固体推进剂燃烧性能模拟计算的神经网络方法[J].推进技术,1996,17(4):72-76.
作者姓名:邓鹏图  田德余  庄逢辰
作者单位:国防科技大学材料科学与应用化学系
摘    要:在总结已有燃烧模型的基础上,重点考虑压强、氧化剂的重均粒径、氧化剂的质量浓度三种主要影响因素,提出了一种基于误差反传(BP)神经网络的复合固体推进剂燃烧性能模拟计算方法,计算结果和实验值吻合较好,这为推进剂配方的计算机辅助设计提供了一种新方法。

关 键 词:神经元机,复合推进剂,推进剂燃速,计算化学

A NEURAL NETWORK FOR MODELING CALCULATIONS FOR COMPOSITE PROPELLANTS
Deng Pengtu,Tian Deyu and Zhuang Fengchen.A NEURAL NETWORK FOR MODELING CALCULATIONS FOR COMPOSITE PROPELLANTS[J].Journal of Propulsion Technology,1996,17(4):72-76.
Authors:Deng Pengtu  Tian Deyu and Zhuang Fengchen
Institution:Dept. of Material Science and Applied Chemistry, National Univ.of Defense Technology, Changsha, 410073;Dept. of Material Science and Applied Chemistry, National Univ.of Defense Technology, Changsha, 410073;Dept. of Material Science and Applied Chemistry, National Univ.of Defense Technology, Changsha, 410073
Abstract:he traditional modeling of composite propellant combustion, which strives to representthe combustion process in mathematical terms, is restricted by the knowledge of the combustionmechanism. In this paper, a new scheme has been proposed to calculate the combustion of compositepropellants without considering the specific combustion processes by applying the back-propagation(BP) neural network, which has the capability to "learn" system characteristics through nonlinearmapping. The computed results are in good agreement with the experimental data, which shows thatthe scheme offers a new way for CAD of propellant formulation.
Keywords:Neural machine  Composite propellant  Propellant burning rate  Computational chemistry
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