首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于遗传神经网络的高能固体推进剂高压燃烧性能计算
引用本文:张小平,代志龙.基于遗传神经网络的高能固体推进剂高压燃烧性能计算[J].固体火箭技术,2007,30(3):229-232.
作者姓名:张小平  代志龙
作者单位:西北工业大学航天学院,西安,710072;中国航天科技集团公司四院四十二所,襄樊,441003
摘    要:建立并利用遗传(GA-BP)神经网络对NEPE类高能固体推进剂高压燃烧性能进行了模拟计算。针对计算需求,对NEPE类高能固体推进剂配方进行了全新表征,提出了13个表征参数。燃速预示结果表明,该方法计算误差小于10%,精度较高,能指导高能固体推进剂高压燃烧性能研究及配方设计;同时,也说明该表征方法能反映出此类配方的本质特征。该研究为高能固体推进剂燃速预估提供了新方法。

关 键 词:高能固体推进剂  燃速预示  遗传神经网络
文章编号:1006-2793(2007)03-0229-04
收稿时间:2006-10-30
修稿时间:2006-10-302006-12-10

Calculation for high-pressure combustion properties of high-energy solid propellant based on GA-BP neural network
ZHANG Xiao-ping,DAI Zhi-long.Calculation for high-pressure combustion properties of high-energy solid propellant based on GA-BP neural network[J].Journal of Solid Rocket Technology,2007,30(3):229-232.
Authors:ZHANG Xiao-ping  DAI Zhi-long
Abstract:A genetic algorithm(GA)-back-propagation(BP)neural network was established.The high-pressure combustion properties of NEPE high-energy solid propellant were simulated and calculated by using the GA-BP neural network.Aiming at calculation requirement,NEPE high-energy solid propellant formulation was characterized,and 13 parameters were put forward.The burning-rate prediction results show that the calculation error of the method is less than 10%,and its accuracy is high;the method can be used for high-pressure combustion property research and formulation design of NEPE high-energy solid propellant.At the same time,the method can reflect essential characteristics of the formulation,and the investigation provides a kind of new method for burning-rate prediction of high-energy solid propellant.
Keywords:high-energy solid propellant  prediction of burning rate  GA-BP neural network
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号