{"title":"Conditions aux limites absorbantes sur des frontières libres","authors":"Azeddine Kourta, Renaud Sauvage","doi":"10.1016/S1620-7742(01)01411-8","DOIUrl":null,"url":null,"abstract":"<div><p>To ensure the exit of vortices from an open computational domain, new boundary conditions for compressible Navier–Stokes equations, called ‘absorbing conditions’, are introduced. They use a layer around computational domain which eliminates nonphysical perturbations. They are compared to three kinds of boundary conditions based on characteristic relations. Computations of two test cases show the best behaviours of the new boundary conditions. These last ones involve a very small perturbation and can be used to solve aeroacoustic problems.</p></div>","PeriodicalId":100302,"journal":{"name":"Comptes Rendus de l'Académie des Sciences - Series IIB - Mechanics","volume":"329 12","pages":"Pages 857-864"},"PeriodicalIF":0.0000,"publicationDate":"2001-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S1620-7742(01)01411-8","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Comptes Rendus de l'Académie des Sciences - Series IIB - Mechanics","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1620774201014118","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2
Abstract
To ensure the exit of vortices from an open computational domain, new boundary conditions for compressible Navier–Stokes equations, called ‘absorbing conditions’, are introduced. They use a layer around computational domain which eliminates nonphysical perturbations. They are compared to three kinds of boundary conditions based on characteristic relations. Computations of two test cases show the best behaviours of the new boundary conditions. These last ones involve a very small perturbation and can be used to solve aeroacoustic problems.