Ziqi 子淇 FANG 方, H. ZONG 宗, Y. Wu 吴, H. Liang 梁, Z. SU 苏
{"title":"基于网格型和超密集阵列等离子体致动器的机翼摩擦阻力减小技术 \"的更正","authors":"Ziqi 子淇 FANG 方, H. ZONG 宗, Y. Wu 吴, H. Liang 梁, Z. SU 苏","doi":"10.1088/2058-6272/ad5d4e","DOIUrl":null,"url":null,"abstract":"\n Figure 4(b) of the paper [Plasma Sci. Technol.\n 26 (2024) 025503] has been corrected. This modification does not affect the result presented in the paper.","PeriodicalId":506986,"journal":{"name":"Plasma Science and Technology","volume":"1 6","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Corrigendum to “Airfoil friction drag reduction based on grid-type and super-dense array plasma actuators”\",\"authors\":\"Ziqi 子淇 FANG 方, H. ZONG 宗, Y. Wu 吴, H. Liang 梁, Z. SU 苏\",\"doi\":\"10.1088/2058-6272/ad5d4e\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"\\n Figure 4(b) of the paper [Plasma Sci. Technol.\\n 26 (2024) 025503] has been corrected. This modification does not affect the result presented in the paper.\",\"PeriodicalId\":506986,\"journal\":{\"name\":\"Plasma Science and Technology\",\"volume\":\"1 6\",\"pages\":\"\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2024-07-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Plasma Science and Technology\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1088/2058-6272/ad5d4e\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Plasma Science and Technology","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1088/2058-6272/ad5d4e","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Corrigendum to “Airfoil friction drag reduction based on grid-type and super-dense array plasma actuators”
Figure 4(b) of the paper [Plasma Sci. Technol.
26 (2024) 025503] has been corrected. This modification does not affect the result presented in the paper.
求助内容：
应助结果提醒方式：
京公网安备 11010802042870号
