Spray characteristics of pintle injector with high gas-liquid momentum ratio

IF 3.4 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE Acta Astronautica Pub Date : 2025-05-01 Epub Date: 2025-02-10 DOI:10.1016/j.actaastro.2025.02.012
Jiaqi Li , Nanjia Yu , Shutao Han , Chuang Zhou , Bowei Jiao
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Abstract

Experimental and numerical simulation methods were employed to investigate the spray characteristics of a pintle injector under high gas-liquid momentum ratio conditions. In the experiments, water and nitrogen were used as the working media. The spray angle and spray modes were investigated using background light imaging and dynamic mode decomposition techniques. Numerical simulations were carried out using a three-dimensional Volume of Fluid to Discrete Particle Model (VOF to DPM) to explore the spray field configuration, Sauter Mean Diameter (SMD) of droplets, and droplet distribution. The results indicate that the spray pattern of the high momentum ratio gas-liquid pintle injector is distinct from that of the traditional hollow cone, presenting as a solid cylindrical spray with reduced size and lower turbulence levels in the recirculation zone. An empirical formula was derived for the spray angle, expressed as θ=32(MWe)0.63, incorporating the Weber number as a significant factor influencing the spray angle. Furthermore, the spray modes were classified into three types based on the gas-liquid momentum ratio (M) and Weber number (We), and their oscillation patterns were analyzed individually. The M was found to significantly influence the droplet diameter and distribution: a higher ratio resulted in a smaller droplet size but also led to droplet accumulation below the injector's central axis, potentially compromising the thermal protection of the pintle tip.
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高气液动量比针状喷射器的喷雾特性
采用实验和数值模拟相结合的方法,研究了高气液动量比条件下针状喷射器的喷雾特性。实验中以水和氮气为工质。利用背景光成像和动态模态分解技术研究了喷雾角度和喷雾模式。采用三维流体体积-离散粒子模型(VOF - to - DPM)进行了数值模拟,探讨了喷雾场的结构、液滴的平均直径(SMD)和液滴的分布。结果表明,高动量比气液针孔喷射器的喷射模式与传统的空心锥喷射器不同,呈现出尺寸减小、再循环区湍流程度降低的固体圆柱形喷雾。考虑韦伯数是影响喷雾角的重要因素,推导出喷雾角的经验公式:θ=32(MWe)−0.63。基于气液动量比(M)和韦伯数(We)将喷雾模式划分为3种,并对其振荡模式进行了分析。研究发现,M对液滴直径和分布有显著影响:较高的比例会导致液滴尺寸变小,但也会导致液滴积聚在喷射器中心轴以下,从而可能损害针尖的热保护。
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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