Simulation Analysis of the Effect of Slit/Slot Pintle Geometry on Atomization of Bipropellant Engine

Author:

Cai Kun1,Zhang Zhen12ORCID,Wang Fengshan1,Hu Yu1,Wang Xudong1ORCID,Fang Zhicheng1,Mao Xiaofang1,Yao Zhaopu1,Yu Yusong2ORCID,Li Haiwang3

Affiliation:

1. Beijing Institute of Control Engineering, Beijing 100190, China

2. Hydrogen Energy and Space Propulsion Laboratory (HESPL), School of Mechanical, Electronic and Control Engineering, Beijing Jiaotong University, Beijing 100044, China

3. Tianmushan Laboratory, Hangzhou 310023, China

Abstract

In order to optimize the slit/slot geometry design of a bipropellant pintle injector, the impinging spray development of a pintle injector was numerically investigated. The VOF (volume of fluid) and LES (large eddy simulation) methods were employed for an analysis to capture the gas–liquid interface by means of the AMR (adaptive mesh refinement) method. In those simulation cases, different flowrates, slot numbers, pintle diameters, slot thicknesses and slot shapes were compared for an analysis. In a comparison of visualization and quantification, a high flowrate and large pintle diameter were shown to be more positive features for improving the atomization quality and mixing effect. As for the slot parameters and shape, the spray development was mainly determined by the flow proportion between the slit jet and slot jet. The simulation results indicated that dominant slot jets cause a more dispersed spatial distribution, which is more conducive to the subsequent improvement of combustion efficiency in a limited space. However, an excessive increase in the number of slot jets can weaken the overall atomization quality and mixing effect, so it is suggested to ensure a balance for geometry design optimization.

Funder

The National Key R&D Program of China

Publisher

MDPI AG

Subject

Process Chemistry and Technology,Chemical Engineering (miscellaneous),Bioengineering

Reference32 articles.

1. Numerical simulation of spray and mixing process of impingement between sheet and jet in pintle injector element;Wang;Acta Aeronaut. Astronaut. Sin.,2020

2. Heister, S.D. (2011). Handbook of Atomization and Sprays: Theory and Applications, Springer Science + Business Media.

3. Dressler, G.A. (2006, January 9–12). Summary of deep throttling rocket engines with emphasis on Apollo LMDE. Proceedings of the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Sacramento, Sacramento, CA, USA.

4. Development of 7500 N variable thrust engine for Chang ′e-3 probe;Lei;Sci. Sin. Technol.,2014

5. Technological advancements and promotion roles of Chang’e-3 lunar probe mission;Sun;Sci. China Technol. Sci.,2013

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