{"title":"可变翼面积的飞机","authors":"S. Osipov, A. V. Tarasenko","doi":"10.37005/1818-0744-2019-3-43-46","DOIUrl":null,"url":null,"abstract":"The paper proposes the idea of a low-altitude aircraft with a variable wing area in flight. Using computational aerodynamics methods, it is shown that the reduction of the wing area as fuel is generated increases the flight range compared to a traditional aircraft with a constant wing area.","PeriodicalId":306467,"journal":{"name":"Bulletin of Dubna International University for Nature, Society, and Man. Series: Natural and engineering sciences","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-12-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"AIRCRAFT WITH VARIABLE WING AREA\",\"authors\":\"S. Osipov, A. V. Tarasenko\",\"doi\":\"10.37005/1818-0744-2019-3-43-46\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper proposes the idea of a low-altitude aircraft with a variable wing area in flight. Using computational aerodynamics methods, it is shown that the reduction of the wing area as fuel is generated increases the flight range compared to a traditional aircraft with a constant wing area.\",\"PeriodicalId\":306467,\"journal\":{\"name\":\"Bulletin of Dubna International University for Nature, Society, and Man. Series: Natural and engineering sciences\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-12-27\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Bulletin of Dubna International University for Nature, Society, and Man. Series: Natural and engineering sciences\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.37005/1818-0744-2019-3-43-46\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Bulletin of Dubna International University for Nature, Society, and Man. Series: Natural and engineering sciences","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.37005/1818-0744-2019-3-43-46","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The paper proposes the idea of a low-altitude aircraft with a variable wing area in flight. Using computational aerodynamics methods, it is shown that the reduction of the wing area as fuel is generated increases the flight range compared to a traditional aircraft with a constant wing area.
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