{"title":"过冷液滴气流中防冰体涂层粗糙度周期的估算","authors":"I. Amelyushkin, Al Miller, A. Stasenko","doi":"10.18384/2310-7251-2021-1-54-63","DOIUrl":null,"url":null,"abstract":"Aim. Geometric properties of ice-phobic surfaces are mathematically simulated to provide the anti-icing effect. Methodology. Numerical calculations of droplet motion in the vicinity of a cylinder simulating the leading edge of a wing relies on the use of previously published mathematical models of physical processes. Results. As applied to the problem of icing of aircrafts, the relief configuration of hydrophobic coatings of a solid is estimated in air flow with supercooled droplets","PeriodicalId":33476,"journal":{"name":"Vestnik moskovskogo gosudarstvennogo oblastnogo universiteta Seriia Fizikamatematika","volume":"19 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2021-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"ESTIMATION OF THE ROUGHNESS PERIOD OF ANTI-ICE BODY COATINGS IN AIR FLOW WITH SUPERCOOLED DROPLETS\",\"authors\":\"I. Amelyushkin, Al Miller, A. Stasenko\",\"doi\":\"10.18384/2310-7251-2021-1-54-63\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Aim. Geometric properties of ice-phobic surfaces are mathematically simulated to provide the anti-icing effect. Methodology. Numerical calculations of droplet motion in the vicinity of a cylinder simulating the leading edge of a wing relies on the use of previously published mathematical models of physical processes. Results. As applied to the problem of icing of aircrafts, the relief configuration of hydrophobic coatings of a solid is estimated in air flow with supercooled droplets\",\"PeriodicalId\":33476,\"journal\":{\"name\":\"Vestnik moskovskogo gosudarstvennogo oblastnogo universiteta Seriia Fizikamatematika\",\"volume\":\"19 1\",\"pages\":\"\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2021-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Vestnik moskovskogo gosudarstvennogo oblastnogo universiteta Seriia Fizikamatematika\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.18384/2310-7251-2021-1-54-63\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Vestnik moskovskogo gosudarstvennogo oblastnogo universiteta Seriia Fizikamatematika","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.18384/2310-7251-2021-1-54-63","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
ESTIMATION OF THE ROUGHNESS PERIOD OF ANTI-ICE BODY COATINGS IN AIR FLOW WITH SUPERCOOLED DROPLETS
Aim. Geometric properties of ice-phobic surfaces are mathematically simulated to provide the anti-icing effect. Methodology. Numerical calculations of droplet motion in the vicinity of a cylinder simulating the leading edge of a wing relies on the use of previously published mathematical models of physical processes. Results. As applied to the problem of icing of aircrafts, the relief configuration of hydrophobic coatings of a solid is estimated in air flow with supercooled droplets