总压力传感器在超声波流中应用,在低压条件下进行冲击波分析
Michal Bílek1, Jiří Maxa1,2, Pavla Šabacká1,2
1Faculty of Electrical Engineering and Communication, Brno University of Technology, Technická 10, 616 00 Brno, Czech Republic.
Sensors (Basel, Switzerland)
|October 29, 2025
概括
一个新的传感器测量了超音速流的总压力. 这项研究验证了近连续冲击波分析的计算流体动力学 (CFD) 模型,这对于环境扫描电子显微镜 (ESEM) 至关重要.
科学领域:
- 流体动力学 流体动力学
- 航空航天工程 航空航天工程
- 物理化学 物理化学
背景情况:
- 超音速流动为准确的压力测量带来独特的挑战.
- 了解连续性极限附近的冲击波行为对于先进的科学仪器来说至关重要.
- 环境扫描电子显微镜 (ESEM) 需要精确控制压力差异.
研究的目的:
- 设计和实施一种传感器,用于测量超音速气流中的总压力.
- 为了描述喷嘴下游的总压力分布,产生正常的冲击波.
- 使用实验数据验证和校准计算流体动力学 (CFD) 模型.
主要方法:
- 使用绝对和差压传感器的组合.
- 在低压状态下进行实验,研究冲击波现象.
- 采用实验结果来改进接近连续力学极限的CFD模型.
主要成果:
- 成功测量了超音速流动中的总压力分布.
- 对近连续冲击波条件的验证的CFD模型.
- 在正常冲击波中,量化的增加是由于扩展的平均自由路径造成的.
结论:
- 开发的传感器是有效的总压力测量在超音速流.
- 经过验证的CFD模型增强了对近连续模式中冲击波的理解.
- 这些发现直接适用于优化ESEM差分室.
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