Jiyu Sun, Ruijuan Du, Chao Liu, Xianping Liu, Zhijun Zhang
{"title":"蜻蜓翅脉结构对飞行特性的影响","authors":"Jiyu Sun, Ruijuan Du, Chao Liu, Xianping Liu, Zhijun Zhang","doi":"10.1109/3M-NANO.2018.8552180","DOIUrl":null,"url":null,"abstract":"The wings of dragonfly have been extensively researched for designing of Micro Air Vehicles (MAVs). The cross-sectional structure of the veins will be influent to flight characteristics of dragonfly. In this paper, elliptical and circular tube structures are found in vein by fluorescence microscope. Based on the results, model I and model II with elliptical and circular cross-sectional structural vein are established, respectively. By computational fluid dynamics (CFD) simulation, the drag coefficient, lift coefficient and lift-to-drag ratio of model I and model II are obtained. It is shown that model I can generate greater lift and produce less resistance. The lift-to-drag ratio of model I is larger 50% than that of model II at an angle of attack of 60 degrees. It will be provided a bioinspiration to design a bionic flapping MAV.","PeriodicalId":6583,"journal":{"name":"2018 IEEE International Conference on Manipulation, Manufacturing and Measurement on the Nanoscale (3M-NANO)","volume":"286 1","pages":"138-141"},"PeriodicalIF":0.0000,"publicationDate":"2018-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Effects of Dragonfly Wing Vein Structure on the Flight Charateristics\",\"authors\":\"Jiyu Sun, Ruijuan Du, Chao Liu, Xianping Liu, Zhijun Zhang\",\"doi\":\"10.1109/3M-NANO.2018.8552180\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The wings of dragonfly have been extensively researched for designing of Micro Air Vehicles (MAVs). The cross-sectional structure of the veins will be influent to flight characteristics of dragonfly. In this paper, elliptical and circular tube structures are found in vein by fluorescence microscope. Based on the results, model I and model II with elliptical and circular cross-sectional structural vein are established, respectively. By computational fluid dynamics (CFD) simulation, the drag coefficient, lift coefficient and lift-to-drag ratio of model I and model II are obtained. It is shown that model I can generate greater lift and produce less resistance. The lift-to-drag ratio of model I is larger 50% than that of model II at an angle of attack of 60 degrees. It will be provided a bioinspiration to design a bionic flapping MAV.\",\"PeriodicalId\":6583,\"journal\":{\"name\":\"2018 IEEE International Conference on Manipulation, Manufacturing and Measurement on the Nanoscale (3M-NANO)\",\"volume\":\"286 1\",\"pages\":\"138-141\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-08-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 IEEE International Conference on Manipulation, Manufacturing and Measurement on the Nanoscale (3M-NANO)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/3M-NANO.2018.8552180\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 IEEE International Conference on Manipulation, Manufacturing and Measurement on the Nanoscale (3M-NANO)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/3M-NANO.2018.8552180","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Effects of Dragonfly Wing Vein Structure on the Flight Charateristics
The wings of dragonfly have been extensively researched for designing of Micro Air Vehicles (MAVs). The cross-sectional structure of the veins will be influent to flight characteristics of dragonfly. In this paper, elliptical and circular tube structures are found in vein by fluorescence microscope. Based on the results, model I and model II with elliptical and circular cross-sectional structural vein are established, respectively. By computational fluid dynamics (CFD) simulation, the drag coefficient, lift coefficient and lift-to-drag ratio of model I and model II are obtained. It is shown that model I can generate greater lift and produce less resistance. The lift-to-drag ratio of model I is larger 50% than that of model II at an angle of attack of 60 degrees. It will be provided a bioinspiration to design a bionic flapping MAV.