Isao Shimoyama, Y. K. Fujisawa, Gregory D. Gekan, H. Miura, Musahito Shimaah, Yoichiro
{"title":"微翼流体动力学","authors":"Isao Shimoyama, Y. K. Fujisawa, Gregory D. Gekan, H. Miura, Musahito Shimaah, Yoichiro","doi":"10.1109/MEMSYS.1995.472567","DOIUrl":null,"url":null,"abstract":"On the other hand, little is known about low Re flow. Therefore, the aerodynamics of low Re flow must be investigated in order to estimate an aerodynamic force on a flying microrobot. Fluid dynamics in low Re flow has been examined experimentally in air and water, and these results are compared to a computer simulation in this paper. The results show that the thrust is sufficient for flight. Fig. 1. Photo of microplane.","PeriodicalId":273283,"journal":{"name":"Proceedings IEEE Micro Electro Mechanical Systems. 1995","volume":"23 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"8","resultStr":"{\"title\":\"Fluid dynamics of microwing\",\"authors\":\"Isao Shimoyama, Y. K. Fujisawa, Gregory D. Gekan, H. Miura, Musahito Shimaah, Yoichiro\",\"doi\":\"10.1109/MEMSYS.1995.472567\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"On the other hand, little is known about low Re flow. Therefore, the aerodynamics of low Re flow must be investigated in order to estimate an aerodynamic force on a flying microrobot. Fluid dynamics in low Re flow has been examined experimentally in air and water, and these results are compared to a computer simulation in this paper. The results show that the thrust is sufficient for flight. Fig. 1. Photo of microplane.\",\"PeriodicalId\":273283,\"journal\":{\"name\":\"Proceedings IEEE Micro Electro Mechanical Systems. 1995\",\"volume\":\"23 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"8\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings IEEE Micro Electro Mechanical Systems. 1995\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MEMSYS.1995.472567\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings IEEE Micro Electro Mechanical Systems. 1995","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MEMSYS.1995.472567","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
On the other hand, little is known about low Re flow. Therefore, the aerodynamics of low Re flow must be investigated in order to estimate an aerodynamic force on a flying microrobot. Fluid dynamics in low Re flow has been examined experimentally in air and water, and these results are compared to a computer simulation in this paper. The results show that the thrust is sufficient for flight. Fig. 1. Photo of microplane.
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