注射角度对超音速燃烧器在低马赫超音速交叉流量结构和混合性能的影响
Lin Zhang1, Jianhan Liang2, Yi Wang3
1Hypersonic Technology Laboratory, National University of Defense Technology, Changsha, 410073, Hunan, China. zhanglin11@nudt.edu.cn.
Scientific reports
|February 5, 2025
概括
燃料注入角度显著影响超音速燃烧器的性能. 倾斜注射提供了更好的反压电阻,但给点火带来了挑战,需要对高超音速车辆进行仔细设计.
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:
- 有效的燃料空气混合对于高超音速空气呼吸车辆至关重要.
- 燃料注入角度是影响混合效率的关键参数.
研究的目的:
- 为了研究燃料注入角度对超音速燃烧器的流量和混合的影响.
- 在低马赫超音速输入下分析流量特征和混合参数.
主要方法:
- 详细比较和分析瞬间和平均流量特征.
- 详细描述重要的混合参数.
主要成果:
- 与横向注射相比,倾斜注射在风侧显示出更强的燃料波动.
- 注射倾斜缩小了反旋转的旋对 (CVP),减少了喷气-空腔相互作用.
结论:
- 倾斜的注射提高了在低马赫超音速交叉流程中的反压阻力.
- 倾斜注入带来了更大的点火挑战,要求对高超音速应用进行细致的设计.
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