在模型固体燃料雷姆喷气式燃烧器中展示燃料PLIF
Applied optics
|September 22, 2025
概括
这项研究通过使用光成像测量燃料蒸气组成,推进了固体燃料雷射技术. 结果有助于校准热解模型和理解可燃性,以提高发动机性能.
科学领域:
- 燃烧科学 燃烧科学
- 航空航天工程 航空航天工程
- 化学工程是化学工程的重要组成部分.
背景情况:
- 固体燃料雷姆喷气 (SFRJ) 的部署受到燃料分解和性能特征的挑战的限制.
- 了解燃料蒸汽动态对于校准热解模型和评估可燃性至关重要.
研究的目的:
- 在SFRJ发动机中使用光成像测量相对燃料混合物分量.
- 研究压力和温度对燃料蒸气组成的影响.
- 对实验数据进行计算流体动力学 (CFD) 模型的验证.
主要方法:
- 利用紫外线激光诱导的光成像来量化单质布他和碳化合物燃料部分.
- 在各种压力和温度流入条件下进行了实验.
- 执行了2D大模拟 (LES) 和3D雷诺兹-平均纳维尔-斯托克斯 (RANS) 模拟,使用物种运输和合气体-固体边界条件.
主要成果:
- 观察到燃料成分随着燃烧器温度升高而单调增加.
- 在不同压力下确定了相对混合物分量的自我相似配置,其中的偏差归因于流.
- 数字模拟显示与实验数据有很好的一致性,尽管 LES 预测过度,而 RANS 预测不足燃料运输.
结论:
- 光成像为SFRJ发动机中燃料蒸汽的特征提供了一种可行的方法.
- 实验和模拟结果为燃料热解和燃烧动态提供了洞察力.
- 需要进一步改进CFD模型,以准确捕捉燃料运输现象.
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