@inproceedings{522fa60ab5bd4e679134b252b45b778b,
title = "MDO application in solid rocket motor design",
abstract = "To solve problems of low efficiency, long period and not handling coupling in solid rocket motor traditional design, multidisciplinary design optimization method of solid rocket motor was specified through comparison of typical MDO method and multi-objective collaborative optimization model of solid rocket motor MDO was constructed. Aiming at computation difficulties of CO, paper put forward some approaches to solve the problem. Finally, to reduce solid rocket motor computation expense, three most important disciplinary approximate analysis model of shell, thermodynamic calculation and interior ballistics model were formulated. This research will be valuable for solid rocket motor design using MDO theory.",
keywords = "CO, Component, Interior ballistics, Netting theory, Solid rocket motor, Thermodynamic calculation",
author = "Hu Kuan and Song Bifeng and Zhan Lin and Li Zhenliang and Chang Xinlong",
year = "2010",
doi = "10.1109/ICIME.2010.5478347",
language = "英语",
isbn = "9781424452644",
series = "ICIME 2010 - 2010 2nd IEEE International Conference on Information Management and Engineering",
pages = "249--253",
booktitle = "ICIME 2010 - 2010 2nd IEEE International Conference on Information Management and Engineering",
note = "2010 2nd IEEE International Conference on Information Management and Engineering, ICIME 2010 ; Conference date: 16-04-2010 Through 18-04-2010",
}