{"title":"模拟部分由渗透性材料制成的三角翼周围的水流","authors":"A. E. Lutsky, A. V. Severin","doi":"10.1134/S0015462824602778","DOIUrl":null,"url":null,"abstract":"<p>Mathematical modeling of a supersonic gas flow around a delta wing is carried out for M = 2. A wing made of a conventional solid material is compared to a wing whose leading edge is made of a porous material with a porosity coefficient of 0.6. The influence of a permeable edge on the flow structure and thermal regime is studied.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"59 4","pages":"1004 - 1015"},"PeriodicalIF":1.0000,"publicationDate":"2024-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Modeling the Flow around a Delta Wing Partially Made of a Permeable Material\",\"authors\":\"A. E. Lutsky, A. V. Severin\",\"doi\":\"10.1134/S0015462824602778\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<p>Mathematical modeling of a supersonic gas flow around a delta wing is carried out for M = 2. A wing made of a conventional solid material is compared to a wing whose leading edge is made of a porous material with a porosity coefficient of 0.6. The influence of a permeable edge on the flow structure and thermal regime is studied.</p>\",\"PeriodicalId\":560,\"journal\":{\"name\":\"Fluid Dynamics\",\"volume\":\"59 4\",\"pages\":\"1004 - 1015\"},\"PeriodicalIF\":1.0000,\"publicationDate\":\"2024-11-07\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Fluid Dynamics\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://link.springer.com/article/10.1134/S0015462824602778\",\"RegionNum\":4,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"MECHANICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Fluid Dynamics","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1134/S0015462824602778","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 0
摘要
对 M = 2 时三角翼周围的超音速气流进行了数学建模。将由传统固体材料制成的机翼与前缘由多孔材料（孔隙率系数为 0.6）制成的机翼进行了比较。研究了透气边缘对流动结构和热状态的影响。
Modeling the Flow around a Delta Wing Partially Made of a Permeable Material
Mathematical modeling of a supersonic gas flow around a delta wing is carried out for M = 2. A wing made of a conventional solid material is compared to a wing whose leading edge is made of a porous material with a porosity coefficient of 0.6. The influence of a permeable edge on the flow structure and thermal regime is studied.
期刊介绍：
Fluid Dynamics is an international peer reviewed journal that publishes theoretical, computational, and experimental research on aeromechanics, hydrodynamics, plasma dynamics, underground hydrodynamics, and biomechanics of continuous media. Special attention is given to new trends developing at the leading edge of science, such as theory and application of multi-phase flows, chemically reactive flows, liquid and gas flows in electromagnetic fields, new hydrodynamical methods of increasing oil output, new approaches to the description of turbulent flows, etc.
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
