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在超音速交叉流中对圆液体喷射原子化的数值模拟
Donglong Zhou1, Yuli Li2, Jianlong Chang3
1Taiyuan Institute of Technology, Taiyuan, 030008, China. zhoudonglong@163.com.
Scientific reports
|July 2, 2025
概括
在超音速交叉流中研究圆形燃料喷气揭示了低比例 (AR) 喷气提供更好的原子化,透和跨度传播. 高AR喷气更容易转移,影响了scramjet设计.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 燃烧科学 燃烧科学
背景情况:
- 喷气式喷气机的燃烧效率取决于燃料的原子化.
- 在超音速横流中注入液体燃料对于scramjet性能至关重要.
- 了解原子化和动力学是scramjet设计的关键.
研究的目的:
- 为了研究超音速横流中圆形液体燃料喷射器的原子化和状特征.
- 为了探索喷嘴面积比 (AR) 对马赫2.85.5的喷气行为的影响.
主要方法:
- 结合水平设置和流体体积 (CLSVOF) 模拟.
- 大模拟 (LES) 用于流建模.
- 适应性网状精制 (AMR) 提高了计算效率.
主要成果:
- 低AR圆喷气体表现出增强的反偏移,更大的透率和更广泛的跨度分布.
- 高AR圆喷气体显示了偏移的增加,透率的减少,以及更窄的跨度传播.
- 与案例AR4.4相比,案例AR0.25显示了42.8%更大的透率和45.1%更大的跨度范围.
结论:
- 喷嘴面积比显著影响超音速交叉流中的液体喷射原子化.
- 优化AR可以提高燃料空气混合和燃烧稳定性.
- 这些发现为改进喷气式喷气机燃料注射策略提供了指导.
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