{"title":"利用自适应网格细化研究激波边界层相互作用下网格分辨率的影响","authors":"M. E. Olsen, Randolph P. Lillard","doi":"10.2514/6.2018-3858","DOIUrl":null,"url":null,"abstract":"Adaptive Mesh Refinement (AMR) promises a much more computationally efficient means to obtain a discrete approximation to a continuous boundary value problem of a specified accuracy than classic isotropic grid refinement. The AMR capability of OVERFLOW is utilized to provide estimates of the exact analytical solutions to problems of interest for turbulence modeling. Predictions of surface pressure and skin friction, essentially the state of stress at the surface, shows little difference with grids believed to be “grid resolved.” Velocity profiles, on the other hand, show marked differences in flows with shocks. The AMR method, as implemented in OVERFLOW 2.2k, appears to provide the ability to produce arbitrarily accurate solutions at a predictable cost much smaller than classic uniform mesh refinement.","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"7 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":"{\"title\":\"Using Adaptive Mesh Refinement to Study Grid Resolution Effects for Shock-Boundary Layer Interactions\",\"authors\":\"M. E. Olsen, Randolph P. Lillard\",\"doi\":\"10.2514/6.2018-3858\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Adaptive Mesh Refinement (AMR) promises a much more computationally efficient means to obtain a discrete approximation to a continuous boundary value problem of a specified accuracy than classic isotropic grid refinement. The AMR capability of OVERFLOW is utilized to provide estimates of the exact analytical solutions to problems of interest for turbulence modeling. Predictions of surface pressure and skin friction, essentially the state of stress at the surface, shows little difference with grids believed to be “grid resolved.” Velocity profiles, on the other hand, show marked differences in flows with shocks. The AMR method, as implemented in OVERFLOW 2.2k, appears to provide the ability to produce arbitrarily accurate solutions at a predictable cost much smaller than classic uniform mesh refinement.\",\"PeriodicalId\":93061,\"journal\":{\"name\":\"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)\",\"volume\":\"7 1\",\"pages\":\"\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-06-24\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"3\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.2514/6.2018-3858\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2514/6.2018-3858","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Using Adaptive Mesh Refinement to Study Grid Resolution Effects for Shock-Boundary Layer Interactions
Adaptive Mesh Refinement (AMR) promises a much more computationally efficient means to obtain a discrete approximation to a continuous boundary value problem of a specified accuracy than classic isotropic grid refinement. The AMR capability of OVERFLOW is utilized to provide estimates of the exact analytical solutions to problems of interest for turbulence modeling. Predictions of surface pressure and skin friction, essentially the state of stress at the surface, shows little difference with grids believed to be “grid resolved.” Velocity profiles, on the other hand, show marked differences in flows with shocks. The AMR method, as implemented in OVERFLOW 2.2k, appears to provide the ability to produce arbitrarily accurate solutions at a predictable cost much smaller than classic uniform mesh refinement.