在巡航飞行模式下，联合翼结构纵向修整造成的升阻比损失

2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD) Pub Date : 2017-10-01 DOI:10.1109/APUAVD.2017.8308773

K. Predachenko, O. Lemko

{"title":"在巡航飞行模式下，联合翼结构纵向修整造成的升阻比损失","authors":"K. Predachenko, O. Lemko","doi":"10.1109/APUAVD.2017.8308773","DOIUrl":null,"url":null,"abstract":"This paper present Lift-to-Drag ratio losses estimation procedure for several configuration of Joined Wing UAVs at cruise flight mode, that actual at initial design stage for comparison or optimization purpose.","PeriodicalId":163267,"journal":{"name":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","volume":"52 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Lift-to-drag ratio losses due to longitudinal trimming in joined wing configuration at cruise flight mode\",\"authors\":\"K. Predachenko, O. Lemko\",\"doi\":\"10.1109/APUAVD.2017.8308773\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper present Lift-to-Drag ratio losses estimation procedure for several configuration of Joined Wing UAVs at cruise flight mode, that actual at initial design stage for comparison or optimization purpose.\",\"PeriodicalId\":163267,\"journal\":{\"name\":\"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)\",\"volume\":\"52 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2017-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/APUAVD.2017.8308773\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/APUAVD.2017.8308773","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 1

摘要

本文给出了几种组合翼无人机在巡航飞行模式下的升阻比损失估算方法，并在初始设计阶段进行了比较和优化。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Lift-to-drag ratio losses due to longitudinal trimming in joined wing configuration at cruise flight mode

This paper present Lift-to-Drag ratio losses estimation procedure for several configuration of Joined Wing UAVs at cruise flight mode, that actual at initial design stage for comparison or optimization purpose.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)

自引率

0.00%

发文量