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[1]赵剑[],谭永华[],陈建华[],等.MDO关键问题及其在液氧/煤油发动机设计中的应用探讨[J].火箭推进,2016,42(06):1-8.
　ZHAO Jian[],TAN Yonghua[],CHEN Jianhua[],et al.Key technological problems and application of MDO in design of LOX/Kerosene liquid rocket engine[J].Journal of Rocket Propulsion,2016,42(06):1-8.
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MDO关键问题及其在液氧/煤油发动机设计中的应用探讨

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 42 期数: 2016年06期 页码: 1-8 栏目: 研究与设计 出版日期: 2016-12-30
Title:
Key technological problems and application of MDO in design of LOX/Kerosene liquid rocket engine
作者:
赵剑[1]; 谭永华[2]; 陈建华[1]; 付平[1]
西安航天动力研究所,陕西西安,710100航天推进技术研究院,陕西西安,710100
Author(s):
ZHAO Jian[1]; TAN Yonghua[2]; CHEN Jianhua[1]; FU Ping[1]
关键词:
多学科设计优化; 液氧/煤油发动机; 关键问题
Keywords:
multidisciplinary design optimization; LOX/Kerosene engine; key technology
分类号:
V434-34
摘要:
多学科设计优化是一种通过充分探索和利用系统的相互作用机制来设计复杂系统及其子系统的方法论,是当前复杂系统工程设计中最活跃的研究领域.大推力液氧/煤油补燃循环发动机设计的多学科本质属性给传统的设计方法带来了新的挑战,在分析液氧/煤油发动机设计的多学科特征基础上,重点讨论了在液氧/煤油发动机设计中应用MDO技术的关键问题,综述了国内外相关领域的研究进展,阐明了在大推力液氧/煤油补燃循环发动机设计中应用MDO的前景.

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备注/Memo

国家863项目2013AA7023021

更新日期/Last Update: 1900-01-01