Analyzing Influence of Ignition Gas Flow Pipe of Igniter on Working Process

Author:

Chang Jiang,Wu Gongping,Wu Haodong,Hao Xuejie

Abstract

Based on gas dynamics and computational fluid dynamics, the numerical simulation of the steady-state flow field of igniter working in the two conditions was conducted with FLUENT. The numerical simulation results were validated by experiments. Influences of ignition gas flow pipe on the igniter's working performance were analyzed on the basis of test validation. The analysis results show that the combustion chamber pressure has atmospheric pressure and that the igniter works with ignition gas flow pipe. The velocity of throat is lower than the speed of sound and the sonic position moves to the position of ignition gas flow pipe; the velocity, pressure and temperature of throat increase; but the flux, pressure and temperature of outlet decrease. Under the different conditions of combustion chamber pressure, the outlet velocity, pressure, temperature and flux have a stable section; but the flux decreases.

Publisher

EDP Sciences

Subject

General Engineering

Reference17 articles.

1. Baudart P, Duthoit V, Harlay J. Numerical Simulation of Cryotechnic Rocket Engine Ignition[C]//Joint Propulsion Conference, 2013

2. Highly resolved numerical simulation of combustion downstream of a rocket engine igniter

3. Popp M, Stanke J. Experimental Investigation of the HM7B Thrust Chamber Start-Up Transient[C]//Joint Propulsion Conference, 2013

4. Cho Yongho, Chang Haengsoo. Hot Firing Tests of Liquid Rocket Engine Using LOX/LNG[C]//AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2013

5. Agostino L D, Biagioni L, Lamberti G. An Ignition Transient Model for Solid Propellant Rocket Motors[C]//Joint Propulsion Conference & Exhibit, 2001

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3