推进技术 ›› 1992, Vol. 13 ›› Issue (6): 6-12.
• • 上一篇 下一篇
陈杰,王克昌,陈启智
发布日期:
Published:
摘要: 在发动机初步设计阶段,要根据对发动机的构型方案进行分析与评价,来选择发动机主要设计参数,并从多个发动机方案中选择最佳方案。作者以液体推进剂火箭发动机为研究对象,建立了一个发动机构型分析与评价软件IRE/CAA。本文阐述了软件LRE/CAA的设计思想,介绍了软件所包括的模块和各个模块的功能,并说明了在软件实现过程中一些问题的处理方法。
关键词: 液体推进剂火箭发动机;构型;软件开发
Abstract: In the preliminary design phase of engine, engine configurations must be analyzed and assessed to choose main design parameters and to select optimal engine scheme from multiple candidates. A configuration analysis and assessment software for liquid propellant rocket engine LRE/CAA has been set up by author. This paper explains the main idea in design thinking of LRE/CAA, introduces, software blocks and their function, and illustrates how to deal with some problems in software realizing process.
Key words: Liqiud rocket engines;Configuration;Software development
陈杰,王克昌,陈启智. 发动机构型分析与评价软件的设计与实现[J]. 推进技术, 1992, 13(6): 6-12.
0 / / 推荐
导出引用管理器 EndNote|Ris|BibTeX
链接本文: http://jpt.tjjsjpt.com/CN/
http://jpt.tjjsjpt.com/CN/Y1992/V13/I6/6
小助手微信:tjjsxzs
公众号:casic-tjjs
《推进技术》手机版