{"title":"压气机翼型探头三维数值模拟分析","authors":"Ju Luo","doi":"10.1109/ICCEE.2009.280","DOIUrl":null,"url":null,"abstract":"A numerical simulation has been done using CFX11.0 to study the effect of an airfoil probe installed at the leading edge of first stage stator in a compressor. Combination of structured and unstructured grids has been used during the calculation. Result shows that blade loading with and without probe is obviously different at 50% height of blade, while the effect at 20% and 80% height of blade is not obvious. The result has proved that probe indeed has an effect on performance of a compressor, and especially on a compressor with a high speed, high pressure ratio .A corresponding test will be done to validate the result and for a further study.","PeriodicalId":343870,"journal":{"name":"2009 Second International Conference on Computer and Electrical Engineering","volume":"14 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2009-12-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Analysis of 3D Numerical Simulation for an Airfoil Probe in a Compressor\",\"authors\":\"Ju Luo\",\"doi\":\"10.1109/ICCEE.2009.280\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A numerical simulation has been done using CFX11.0 to study the effect of an airfoil probe installed at the leading edge of first stage stator in a compressor. Combination of structured and unstructured grids has been used during the calculation. Result shows that blade loading with and without probe is obviously different at 50% height of blade, while the effect at 20% and 80% height of blade is not obvious. The result has proved that probe indeed has an effect on performance of a compressor, and especially on a compressor with a high speed, high pressure ratio .A corresponding test will be done to validate the result and for a further study.\",\"PeriodicalId\":343870,\"journal\":{\"name\":\"2009 Second International Conference on Computer and Electrical Engineering\",\"volume\":\"14 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2009-12-28\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2009 Second International Conference on Computer and Electrical Engineering\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICCEE.2009.280\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2009 Second International Conference on Computer and Electrical Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICCEE.2009.280","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Analysis of 3D Numerical Simulation for an Airfoil Probe in a Compressor
A numerical simulation has been done using CFX11.0 to study the effect of an airfoil probe installed at the leading edge of first stage stator in a compressor. Combination of structured and unstructured grids has been used during the calculation. Result shows that blade loading with and without probe is obviously different at 50% height of blade, while the effect at 20% and 80% height of blade is not obvious. The result has proved that probe indeed has an effect on performance of a compressor, and especially on a compressor with a high speed, high pressure ratio .A corresponding test will be done to validate the result and for a further study.
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
