引用本文:
【打印本页】   【HTML】 【下载PDF全文】   查看/发表评论  【EndNote】   【RefMan】   【BibTex】
←前一篇|后一篇→ 过刊浏览    高级检索
本文已被:浏览 1240次   下载 538 本文二维码信息
码上扫一扫!
分享到: 微信 更多
电热式热交换器的数值分析
祖国君, 王慧玉
北京航空航天大学
摘要:
对工质加热以提高其比冲,是电火箭应用中的一个技术问题。本文对圆环形通道的内加热流动问题进行了研究。应用Patanka-Spardlinq方法,求解了抛物型的N-S方程,并考虑了外壁面的散热损失。对不同氨分解率和膨胀比的多种情况进行了计算,并对热功率和管道长度的选择进行了分析。
关键词:  电火箭发动机  电加热  热交换器  数值分析
DOI:
分类号:
基金项目:
NUMERICAL ANALYSIS OF ELECTRIC HEAT EXCHANGER
Zhu Guojun, Wang Huiyu
Beijing University of Aeronautics and Astronautics
Abstract:
For the improvement of the specific impulsion in electric rocket, the heating of actuating medium with elctric power is a practical method. In this paper, the flow in a annular passage is investigated. The Patankar-Spalding method is used to solve the parabolic Navier-Stokes equations and the heat losses at the outer wall is considered.Calculations are performed for various ammonia decomposition rates and various nozzle expand ratio, and the selection of heat power and passage length are investigated also.
Key words:  Electric rocket engine  Electric heating  Heat exchanger  Numerical analysis