| 喷管性能计算的软件实现 |
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| 引用本文： | 孙得川,陈杰,刘昌国,林庆国.喷管性能计算的软件实现[J].上海航天,2002,19(6):18-20,50. |
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| 作者姓名： | 孙得川 陈杰 刘昌国 林庆国 |
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| 作者单位： | 1. 西北工业大学,航天工程学院,陕西,西安,710072
2. 上海航天技术研究院801所,上海,200233 |
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| 摘 要： | 基于化学平衡和化学动力学理论，用C^ 和FORTRAN编写了液体火箭发动机喷管性能一维计算软件，软件建立了相关的推进剂数据和化学反应数据库，使计算很简便，针对某型号发动机进行计算，得到了特定条件下发动机的性能参数和化学动力学损失等。
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| 关 键 词： | 化学平衡 化学动力学 喷管性能 液体火箭发动机 计算软件 |
| 文章编号： | 1006-1630(2002)06-0018-03 |
Software of One-Dimensional Nozzle Performance Calculation |
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| SUN De chuan ,CHEN Jie ,LIU Chang guo ,LIN Qing guo.Software of One-Dimensional Nozzle Performance Calculation[J].Aerospace Shanghai,2002,19(6):18-20,50. |
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| Authors: | SUN De chuan CHEN Jie LIU Chang guo LIN Qing guo |
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| Institution: | SUN De chuan 1,CHEN Jie 2,LIU Chang guo 2,LIN Qing guo 2 |
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| Abstract: | Based on the theory of chemical equilibrium and kinetic methods, one software for one dimensional nozzle performance calculation written by C++ and FORTRAN is introduced in this paper. In the software, databases are built for propellants and chemical reaction, which simplify the calculation procedure. In a computation example of some engine, the performances of the nozzle and the kinetic loss for the engine are obtained under certain conditions. |
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| Keywords: | Chemical equilibrium Chemical kinetics Nozzle performance |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
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