{"title":"直升机叶片DNW (NLR)附近二维激光测速","authors":"A. Boutier, J. Lefèvre, D. Soulevant, F. Dunand","doi":"10.1109/ICIASF.1993.687675","DOIUrl":null,"url":null,"abstract":"Tests achieved at DNW (windtunnel of NLR) on an helicopter in forward flight conditions had two main purposes: on the one hand to record the components of the velocity vector in a 2D vertical frame around the blade, and on the other hand to simultaneously measure the position of the 2 m long blade which is rotating at a speed of 1050 rpm. Two series of measurements have been performed: the first one in a closed test section (8 m x 10 m) with a working distance of 2.7 m, the second one in an open test section for which this working distance was increased up to 5 m. The optical and mechanical set-up, the synchronization of the measurements and the blade attitude measurement technique are described; the: most typical results are presented.","PeriodicalId":398832,"journal":{"name":"International Congress on Instrumentation in Aerospace Simulation Facilities,","volume":"4 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-09-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":"{\"title\":\"2D Laser Velocimetry Near Helicopter Blades in DNW (NLR)\",\"authors\":\"A. Boutier, J. Lefèvre, D. Soulevant, F. Dunand\",\"doi\":\"10.1109/ICIASF.1993.687675\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Tests achieved at DNW (windtunnel of NLR) on an helicopter in forward flight conditions had two main purposes: on the one hand to record the components of the velocity vector in a 2D vertical frame around the blade, and on the other hand to simultaneously measure the position of the 2 m long blade which is rotating at a speed of 1050 rpm. Two series of measurements have been performed: the first one in a closed test section (8 m x 10 m) with a working distance of 2.7 m, the second one in an open test section for which this working distance was increased up to 5 m. The optical and mechanical set-up, the synchronization of the measurements and the blade attitude measurement technique are described; the: most typical results are presented.\",\"PeriodicalId\":398832,\"journal\":{\"name\":\"International Congress on Instrumentation in Aerospace Simulation Facilities,\",\"volume\":\"4 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1993-09-20\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"3\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Congress on Instrumentation in Aerospace Simulation Facilities,\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICIASF.1993.687675\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Congress on Instrumentation in Aerospace Simulation Facilities,","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICIASF.1993.687675","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
2D Laser Velocimetry Near Helicopter Blades in DNW (NLR)
Tests achieved at DNW (windtunnel of NLR) on an helicopter in forward flight conditions had two main purposes: on the one hand to record the components of the velocity vector in a 2D vertical frame around the blade, and on the other hand to simultaneously measure the position of the 2 m long blade which is rotating at a speed of 1050 rpm. Two series of measurements have been performed: the first one in a closed test section (8 m x 10 m) with a working distance of 2.7 m, the second one in an open test section for which this working distance was increased up to 5 m. The optical and mechanical set-up, the synchronization of the measurements and the blade attitude measurement technique are described; the: most typical results are presented.