{"title":"用于测量低速流中三个平均速度分量的微型五孔压力探头","authors":"P. Ligrani, B. Singer, L. Baun","doi":"10.1088/0022-3735/22/10/013","DOIUrl":null,"url":null,"abstract":"A miniature five-hole pressure probe is described which has a probe tip diameter of 1.22 mm. The probe was developed to measure three mean velocity components using a non-nulling procedure at individual locations in a curved channel where differential pressures are low, flow is three-dimensional and laminar, and spatial resolution and flow blockage effects are important considerations. Calibration coefficients are presented for Reynolds numbers based on probe tip diameter ranging from 80 to 400. Coefficients for yaw angle, pitch angle, total pressure and total minus static pressure are independent of Reynolds number within experimental uncertainties. Experimental details unique to the use of the miniature probe are also given along with distributions of mean velocity and mean vorticity over a portion of the 12.7 mm*508.0 mm cross section of a curved channel. At a Dean number of 119 (mean streamwise velocity approximately 1.2 m s-1), structural characteristics of Dean vortices are evident from contours of the streamwise velocity, the total pressure and the streamwise component of mean vorticity determined from secondary flow vectors.","PeriodicalId":16791,"journal":{"name":"Journal of Physics E: Scientific Instruments","volume":"32 1","pages":"868-876"},"PeriodicalIF":0.0000,"publicationDate":"1989-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"62","resultStr":"{\"title\":\"Miniature five-hole pressure probe for measurement of three mean velocity components in low-speed flows\",\"authors\":\"P. Ligrani, B. Singer, L. Baun\",\"doi\":\"10.1088/0022-3735/22/10/013\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A miniature five-hole pressure probe is described which has a probe tip diameter of 1.22 mm. The probe was developed to measure three mean velocity components using a non-nulling procedure at individual locations in a curved channel where differential pressures are low, flow is three-dimensional and laminar, and spatial resolution and flow blockage effects are important considerations. Calibration coefficients are presented for Reynolds numbers based on probe tip diameter ranging from 80 to 400. Coefficients for yaw angle, pitch angle, total pressure and total minus static pressure are independent of Reynolds number within experimental uncertainties. Experimental details unique to the use of the miniature probe are also given along with distributions of mean velocity and mean vorticity over a portion of the 12.7 mm*508.0 mm cross section of a curved channel. At a Dean number of 119 (mean streamwise velocity approximately 1.2 m s-1), structural characteristics of Dean vortices are evident from contours of the streamwise velocity, the total pressure and the streamwise component of mean vorticity determined from secondary flow vectors.\",\"PeriodicalId\":16791,\"journal\":{\"name\":\"Journal of Physics E: Scientific Instruments\",\"volume\":\"32 1\",\"pages\":\"868-876\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1989-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"62\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of Physics E: Scientific Instruments\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1088/0022-3735/22/10/013\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Physics E: Scientific Instruments","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1088/0022-3735/22/10/013","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 62
摘要
描述了一种微型五孔压力探头,探头尖端直径为1.22 mm。该探头用于测量弯曲通道中不同位置的三个平均速度分量,其中压差低,流动是三维和层流的,空间分辨率和流动阻塞效应是重要的考虑因素。给出了基于探头尖端直径范围为80 ~ 400的雷诺数的校正系数。在实验不确定度范围内,横摆角、俯仰角、总压和总负静压的系数与雷诺数无关。实验细节独特的微型探头的使用也给出了平均速度和平均涡量的分布在12.7毫米*508.0毫米的弯曲通道的横截面的一部分。在Dean数为119时(平均流速度约为1.2 m s-1),从二次流矢量确定的流速度、总压和平均涡量的流向分量的等高线可以明显看出Dean涡的结构特征。
Miniature five-hole pressure probe for measurement of three mean velocity components in low-speed flows
A miniature five-hole pressure probe is described which has a probe tip diameter of 1.22 mm. The probe was developed to measure three mean velocity components using a non-nulling procedure at individual locations in a curved channel where differential pressures are low, flow is three-dimensional and laminar, and spatial resolution and flow blockage effects are important considerations. Calibration coefficients are presented for Reynolds numbers based on probe tip diameter ranging from 80 to 400. Coefficients for yaw angle, pitch angle, total pressure and total minus static pressure are independent of Reynolds number within experimental uncertainties. Experimental details unique to the use of the miniature probe are also given along with distributions of mean velocity and mean vorticity over a portion of the 12.7 mm*508.0 mm cross section of a curved channel. At a Dean number of 119 (mean streamwise velocity approximately 1.2 m s-1), structural characteristics of Dean vortices are evident from contours of the streamwise velocity, the total pressure and the streamwise component of mean vorticity determined from secondary flow vectors.