Hypergolic Ignition by Off-Center Binary Collision of Monoethanolamine-NaBH4 and Hydrogen Peroxide Droplets

Author:

Zhang Dawei1,Song Siduo1,Yu Dehai2,Yuan Yueming2,Liu Hongmei13ORCID,Liu Xuedong1ORCID,Fan Xuejun2

Affiliation:

1. School of Mechanical Engineering and Rail Transit, Changzhou University, Changzhou 213164, China

2. State Key Laboratory of High Temperature Gas Dynamics, Chinese Academy of Sciences, Beijing 100190, China

3. Jiangsu Province Engineering Research Center of Intelligent Manufacturing Technology for the New Energy Vehicle Power Battery, Changzhou 213164, China

Abstract

Hypergolic ignition of H2O2 and MEA-NaBH4 by off-center collision of their droplets was experimentally studied, focusing on the characteristics and mechanism of droplet mixing, droplet heating and evaporation, and gas-phase ignition. The whole collision ignition process was divided into five stages, which were compared, respectively, with that of head-on collision. Under the condition of a slightly off-center collision (for cases where B < 0.35), H2O2 droplets penetrate MEA-NaBH4 droplets after the collision and coalesce with it, but the internal H2O2 drop inside the MEA-NaBH4 droplet does not form a stable sphere. Instead, it rotates and expands inside the mixed droplet. With B increasing to 0.59, the droplets no longer coalesce after collision but separate away, forming satellite droplets. In such cases, multi-ignition mode is observed. When B increases to a certain extent, specifically, 0.85, a grazing collision is observed such that no mass transfer exists during the interaction of droplets, which leads to ignition failure. A theoretical model quantifying droplet swelling rate was established to calculate the volume change of the droplet. It was found that the swelling can be attributed to the flash boiling of superheated internal H2O2 fluid. Meanwhile, the ignition delay time was found to linearly decrease with B at various Wes until the extent where the chemical reaction takes over control, leading to an almost constant time delay defined as RDT. Additionally, the regime of ignition modes corresponding to different droplet mixing features is summarized in the We-B parametric space.

Funder

Changzhou University Research Start-up Fund

Changzhou Leading Innovative Talent Project

Natural Science Foundation of Jiangsu Province

Jiangsu Province Engineering Research Center of Intelligent Manufacturing Technology for the New Energy Vehicle Power Battery

Publisher

MDPI AG

Reference32 articles.

1. Fletcher, E.A., and Morrell, G. (1960). Progress in Combustion Science and Technology, Elsevier.

2. Yang, V., Habiballah, M., Hulka, J., and Popp, M. (2004). Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis, and Design, American Institute of Aeronautics and Astronautics, Inc.

3. Sutton, G.P., and Biblarz, O. (2016). Rocket Propulsion Elements, John Wiley & Sons.

4. Hypergolic ignition by head-on collision of N, N, N’, N’−tetramethylethylenediamine and white fuming nitric acid droplets;Zhang;Combust. Flame,2016

5. Kumar, S.K.V., and Frederick, R.A. (2020, January 24–26). Experimental Investigation of Spray Characteristics for Different Geometrical Misalignment Cases of Like Doublet Impinging Injector. Proceedings of the AIAA Propulsion and Energy 2020 Forum, Online.

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