| 高速气流场燃油雾化液滴分布数值研究 |
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| 引用本文： | 马天举,栾希亭,洪流.高速气流场燃油雾化液滴分布数值研究[J].火箭推进,2009,35(3):21-25. |
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| 作者姓名： | 马天举 栾希亭 洪流 |
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| 作者单位： | 1. 西安航天动力研究所,陕西,西安,710100
2. 航天推进技术研究院,陕西,西安,710100 |
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| 摘 要： | 针对亚燃冲压发动机燃烧室内部流动特点,结合二元稳定器试验台高速气流场燃油雾化特性试验,建立试验件三维模型并对其喷雾两相流动进行数值模拟。主要研究了来流马赫数以及喷嘴条件变化时燃油雾化液滴与油气比的分布。分析认为,来流马赫数的增加使得雾化特征角缩小,可同时改善燃油蒸发并获得更加均匀的油气比分布。随着供油压力的提高,离心式与直流式喷嘴雾化特征角均增大,但供油压力不是影响直流喷嘴雾化锥角的主要因素。计算结果与试验结果对比定性符合良好,定量误差范围可以接受,验证了计算模型与计算方法的正确性,所得到的结果可应用于工程设计。
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| 关 键 词： | 亚燃冲压发动机 燃油雾化 燃料分布 雾化角 数值模拟 |
Numerical investigation of spray in high speed airflow |
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| Ma Tianju,Luan Xiting,Hong Liu.Numerical investigation of spray in high speed airflow[J].Journal of Rocket Propulsion,2009,35(3):21-25. |
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| Authors: | Ma Tianju Luan Xiting Hong Liu |
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| Institution: | 1 Xi'an Aerospace Propulsion Institute;Xi'an 710100;China;2 Academy of Aerospace Propulsion Technology;China |
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| Abstract: | Based on experimental investigation of the liquid fuel atomization in high speed airflow and the flow characteristics of ramjet combustion chamber,a three-dimensional model was established.With the two-phase flow numerical simulation,spray field and fuel-air ratio distributions were investigated at different Mach numbers and injector conditions.The simulation results indicate that with the Mach number increasing,an improved vaporization and better fuel distribution were obtained,the atomization angle was re... |
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| Keywords: | ramjet atomization fuel distribution atomization angle numerical simulation model |
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