低密度空气的动力粘度的实验估计使用光学衍生的宏观的短暂流量参数
1Space Research Centre of Polish Academy of Sciences, 00-716 Warsaw, Poland.
Sensors (Basel, Switzerland)
|September 19, 2025
概括
这项研究引入了一种新的方法来计算稀释空气中的动力粘度,使用降落振荡. 这种技术提供了一种简单的方法来测量大气参数,并有助于设计重新进入装置.
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
- 大气科学 大气科学
背景情况:
- 精确测量动力粘度对于理解稀释大气条件至关重要.
- 确定动力粘度的传统方法可能很复杂,需要专门的实验室设备.
研究的目的:
- 提出一种用于计算稀释空气中的动力粘度的新型实验方法.
- 通过平流层气球任务的数据来验证该方法.
- 评估该方法对现实世界大气调查的适用性.
主要方法:
- 在平流层重新进入时,对降落罩振荡的光学记录.
- 对记录的数据进行分析,以确定罗什科和雷诺兹数.
- 应用一种适应式来计算动力粘度.
主要成果:
- 实验方法成功计算了稀释空气的动力粘度.
- 计算的值与现有的实验室文献数据有很好的一致性.
- 识别和讨论了差异的来源.
结论:
- 覆盖式呼吸方法为确定稀释空气中的动力粘度提供了一种可访问的方法.
- 这种方法可以用于研究大气参数和电离层质量流.
- 该技术对于降落和再入境装置的设计和性能验证是有价值的.
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