{"title":"低温风洞和常规风洞的先进力加热技术","authors":"B. Ewald","doi":"10.1109/ICIASF.1993.687648","DOIUrl":null,"url":null,"abstract":"For airplane development and for basic aerodynamic research as well force testing is the main task in the wind tunnel. Rising requirements for accuracy resulted in continous development and improvement of force testing technology. The concept of the cryogenic wind tunnel is an additional challenge for the force balance. At least the same accuracy as in conventional tunnels is requested over a range of 200 Kelvin.","PeriodicalId":398832,"journal":{"name":"International Congress on Instrumentation in Aerospace Simulation Facilities,","volume":"19 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-09-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Advanced Force Teating Technology for Cryogenic and Conventional Wind Tunnels\",\"authors\":\"B. Ewald\",\"doi\":\"10.1109/ICIASF.1993.687648\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"For airplane development and for basic aerodynamic research as well force testing is the main task in the wind tunnel. Rising requirements for accuracy resulted in continous development and improvement of force testing technology. The concept of the cryogenic wind tunnel is an additional challenge for the force balance. At least the same accuracy as in conventional tunnels is requested over a range of 200 Kelvin.\",\"PeriodicalId\":398832,\"journal\":{\"name\":\"International Congress on Instrumentation in Aerospace Simulation Facilities,\",\"volume\":\"19 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1993-09-20\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Congress on Instrumentation in Aerospace Simulation Facilities,\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICIASF.1993.687648\",\"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.1993.687648","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Advanced Force Teating Technology for Cryogenic and Conventional Wind Tunnels
For airplane development and for basic aerodynamic research as well force testing is the main task in the wind tunnel. Rising requirements for accuracy resulted in continous development and improvement of force testing technology. The concept of the cryogenic wind tunnel is an additional challenge for the force balance. At least the same accuracy as in conventional tunnels is requested over a range of 200 Kelvin.
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