Effect of flash boiling on the spray characteristics of pressure swirl spray nozzles using liquid nitrogen

IF 1 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Yihong Lu, Xuesen Yang, Binglong Zhang, Wei Zhao, Bin Hu, Qingjun Zhao
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Abstract

Liquid nitrogen is a widely utilized effective low-temperature cooling medium, also employed in the ATR-GG (Gas Generator cycle Air Turbo rocket) engine to cool high-temperature components. Due to the high-temperature work environment and the ease with which liquid nitrogen evaporates and boils, liquid nitrogen would experience a flash boiling process. In order to study the influence of flash boiling on spray characteristics, experiments and simulations were conducted with two types of hollow-cone nozzles and two types of solid-cone nozzles under subcooled water at normal temperature which is not affect by flash boiling and superheat liquid nitrogen inflow conditions. The research found that flashing already begins inside the nozzle, significantly reducing the discharge coefficient of the solid-cone nozzle. The nitrogen gas-liquid mixture fills the air core of the hollow-cone spray, resulting in a comparatively smaller impact on the discharge coefficient. The liquid nitrogen spray exhibit spray collapse, unable to achieve the spray cone angels as the water spray. The major reason is that during the flashing process, nitrogen vapor expansion enhances the axial velocity, reducing the spray cone angle. The study recommends using hollow-cone nozzles to mitigate the impact of flash boiling on the spray characteristics.
闪沸对使用液氮的压力漩涡喷嘴喷雾特性的影响
液氮是一种广泛使用的有效低温冷却介质,ATR-GG(气体发生器循环空气涡轮火箭)发动机也采用液氮来冷却高温部件。由于工作环境温度高,液氮容易蒸发和沸腾,液氮会经历闪沸过程。为了研究闪沸对喷雾特性的影响,在不受闪沸影响的常温过冷水和过热液氮流入条件下,对两种空心锥形喷嘴和两种实心锥形喷嘴进行了实验和模拟。研究发现,喷嘴内部已经开始闪蒸,大大降低了固体锥形喷嘴的放电系数。氮气-液态混合物充满了空心锥形喷嘴的气芯,对放电系数的影响相对较小。液氮喷雾表现出喷雾塌陷,无法达到与水喷雾一样的喷雾锥角。主要原因是在闪蒸过程中,氮气蒸气膨胀提高了轴向速度,减小了喷雾锥角。研究建议使用空心锥喷嘴来减轻闪沸对喷雾特性的影响。
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来源期刊
CiteScore
2.40
自引率
18.20%
发文量
212
审稿时长
5.7 months
期刊介绍: The Journal of Aerospace Engineering is dedicated to the publication of high quality research in all branches of applied sciences and technology dealing with aircraft and spacecraft, and their support systems. "Our authorship is truly international and all efforts are made to ensure that each paper is presented in the best possible way and reaches a wide audience. "The Editorial Board is composed of recognized experts representing the technical communities of fifteen countries. The Board Members work in close cooperation with the editors, reviewers, and authors to achieve a consistent standard of well written and presented papers."Professor Rodrigo Martinez-Val, Universidad Politécnica de Madrid, Spain This journal is a member of the Committee on Publication Ethics (COPE).
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