PDF下载 分享
[1]黄伟,罗世彬,王振国,等.火箭基组合循环(RBCC)发动机性能分析[J].火箭推进,2007,33(05):6-10.
　Huang Wei,Luo Shibin,Wang Zhenguo.Performance analysis of RBCC engine[J].Journal of Rocket Propulsion,2007,33(05):6-10.
点击复制

火箭基组合循环(RBCC)发动机性能分析

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 33 期数: 2007年05期 页码: 6-10 栏目: 研究与设计 出版日期: 2007-10-30
Title:
Performance analysis of RBCC engine
作者:
黄伟；罗世彬；王振国；
国防科技大学航天与材料工程学院；国防科技大学航天与材料工程学院湖南长沙；410073；湖南长沙；
Author(s):
Huang Wei; Luo Shibin; Wang Zhenguo
Inst.of Aerospace and Material Engineering,National Univ.of Defense Technology,ChangSha 410073,China
关键词:
RBCC; 引射火箭模式; 推力; 推力增益; 比冲
分类号:
V430
文献标志码:
A
摘要:
介绍了采用引射火箭模式的RBCC发动机工作原理,并在对其概念设计模型进行简化的基础上,进行了RBCC发动机系统性能分析,评估了RBCC发动机系统主要设计参数(发动机系统出口截面直径和燃料化学反应后的总温)的变化对其性能(推力、推力系数和比冲)的影响,认为:1)燃料经过加热后,推力和推力增益都上升了69.97%,比冲增加了180.18%;2)随着二次燃烧过程中燃烧室温度的上升,发动机的推力、推力增益和比冲得到了很大的提高,火箭发动机的性能得到了很好的改善;3)随着RBCC发动机系统出口截面直径的增加,尾气对

相似文献/References:

[1]李永洲,刘晓伟,张蒙正,等.马赫数2.5~7.0的二元变几何进气道设计[J].火箭推进,2015,41(05):17.
　LI Yongzhou,LIU Xiaowei,ZHANG Mengzheng,et al.Design of a two dimensional variable geometry inlet with Mach number 2.5~7.0[J].Journal of Rocket Propulsion,2015,41(05):17.
[2]张蒙正,张 玫,严俊峰,等.RBCC动力系统工作模态问题[J].火箭推进,2015,41(02):1.
　ZHANG Meng-zheng,ZHANG Mei,YAN Jun-feng,et al.Discussion about work modal of RBCC power system[J].Journal of Rocket Propulsion,2015,41(05):1.
[3]王洪信,徐 旭.火箭基组合循环发动机性能迭代算法研究[J].火箭推进,2015,41(01):56.
　WANG Hong-xin,XU Xu.Research on performance iterative algorithm of rocket based combined cycle engine[J].Journal of Rocket Propulsion,2015,41(05):56.
[4]张蒙正,李 斌,王 君,等.关于RBCC动力系统的思考[J].火箭推进,2013,39(01):1.
　ZHANG Meng-zheng,LI Bin,WANG Jun,et al.Thinking about RBCC propulsion system[J].Journal of Rocket Propulsion,2013,39(05):1.
[5]路媛媛,张蒙正,严俊峰.火箭推力室喷管内激波对RBCC性能影响分析[J].火箭推进,2013,39(05):46.
　LU Yuan-yuan,ZHANG Meng-zheng,YAN Jun-feng.Influences of shock wave in rocket nozzle on RBCC performance[J].Journal of Rocket Propulsion,2013,39(05):46.
[6]燕 珂,单世群,王莉红,等.液体推进剂热稳定性研究方法探讨[J].火箭推进,2014,40(02):90.
　ZHANG Meng-zheng,LI-Bin,LU Yuan-yuan.Thinking about thrust and resistance characteristics of RBCC power system adapting to rectangle section flow passage[J].Journal of Rocket Propulsion,2014,40(05):90.
[7]安佳宁,徐万武.RBCC引射模态冷流试验研究[J].火箭推进,2012,38(04):38.
　AN Jia-ning,XU Wan-wu.Cold flow experimental research of RBCC ejector modal[J].Journal of Rocket Propulsion,2012,38(05):38.
[8]刘永兴,王 魁,曹再勇.RBCC推进系统主火箭发动机气氧/煤油推力室研究[J].火箭推进,2009,35(06):23.
　Liu Yongxing,Wang Kui,Cao Zaiyong.Investigation of GO2/kerosene thrust chamber of the main rocket engine for the RBCC propulsion system[J].Journal of Rocket Propulsion,2009,35(05):23.
[9]张蒙正,李平,陈祖奎.组合循环动力系统面临的挑战及前景[J].火箭推进,2009,35(01):1.
　Zhang Mengzheng,Li Ping,Chen Zukui.Challenge and perspective of combined cycle propulsion system[J].Journal of Rocket Propulsion,2009,35(05):1.
[10]张留欢,杜泉,张蒙正.RBCC发动机火箭-冲压模态理想热力循环优化分析[J].火箭推进,2016,42(03):21.
　ZHANG Liuhuan,DU Quan,ZHANG Mengzheng.Optimum analysis on ideal thermodynamic cycle of RBCC engine at special rocket-ramjet mode[J].Journal of Rocket Propulsion,2016,42(05):21.

更新日期/Last Update: 1900-01-01