| 发动机构型分析与评价软件的设计与实现 |
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| 引用本文： | 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): 6-12,5 |
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| 作者姓名： | 陈杰 王克昌 陈启智 |
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| 作者单位： | 国防科学技术大学(陈杰，王克昌)，国防科学技术大学(陈启智) |
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| 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。
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| 关 键 词： | 液体推进剂 火箭发动机 程序设计 |
DESIGN AND REALIZATION OF ENGINE CONFIGURATION ANALYSIS AND ASSESSMENT SOFTWARE |
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| Chen Jie,Wg Kechang and Chen Qizhi. DESIGN AND REALIZATION OF ENGINE CONFIGURATION ANALYSIS AND ASSESSMENT SOFTWARE[J]. Journal of Propulsion Technology, 1992, 13(6): 6-12,5 |
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| Authors: | Chen Jie Wg Kechang Chen Qizhi |
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| Affiliation: | National University of Defence Technology |
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| 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. |
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| Keywords: | Liqiud rocket engines Configuration Software development |
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