{"title":"AGARD-B模型下超声速气体流动计算结果","authors":"A. Panasenko","doi":"10.33257/phchgd.21.2.887","DOIUrl":null,"url":null,"abstract":"The article presents the results of calculating the aerodynamic characteristics for a supersonic gas flow around the AGARD-B vehicle model at Mach numbers 4 and 5.1 in the range of angles-of-attack 4÷ 9.19.","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"136 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Results of Supersonic Gas Flow Calculations near AGARD-B Model\",\"authors\":\"A. Panasenko\",\"doi\":\"10.33257/phchgd.21.2.887\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The article presents the results of calculating the aerodynamic characteristics for a supersonic gas flow around the AGARD-B vehicle model at Mach numbers 4 and 5.1 in the range of angles-of-attack 4÷ 9.19.\",\"PeriodicalId\":309290,\"journal\":{\"name\":\"Physical-Chemical Kinetics in Gas Dynamics\",\"volume\":\"136 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Physical-Chemical Kinetics in Gas Dynamics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.33257/phchgd.21.2.887\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Physical-Chemical Kinetics in Gas Dynamics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.33257/phchgd.21.2.887","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Results of Supersonic Gas Flow Calculations near AGARD-B Model
The article presents the results of calculating the aerodynamic characteristics for a supersonic gas flow around the AGARD-B vehicle model at Mach numbers 4 and 5.1 in the range of angles-of-attack 4÷ 9.19.
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