{"id":23059,"date":"2025-10-25T14:29:42","date_gmt":"2025-10-25T14:29:42","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=23059"},"modified":"2025-10-25T14:29:43","modified_gmt":"2025-10-25T14:29:43","slug":"validation-of-an-automated-toolset-for-mesh-adapted-navier-stokes-simulation-of-high-speed-vehicles-using-dns-and-experiment","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/10\/25\/validation-of-an-automated-toolset-for-mesh-adapted-navier-stokes-simulation-of-high-speed-vehicles-using-dns-and-experiment\/","title":{"rendered":"Validation of an automated toolset for mesh adapted Navier-Stokes simulation of high speed vehicles using DNS and experiment"},"content":{"rendered":"\n<p><strong>Mathieu LUGRIN, Baptiste ISNARD, Bruno MAUGARS, Cedric CONTENT<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2025-074<\/strong><\/p>\n\n\n\n<p>A fully automated toolset for Navier-Stokes and Reynolds Averaged Navier-Stokes computation around high speed vehicles is presented. It is based on a CAD-based automated meshing and anisotropic metric-based remeshing tool built on the REFINE toolbox, a node-centered Navier-Stokes in the SoNICS suite, and the maia library. The tool is validated on open cases representative of the complexity of the flow encountered around high-speed vehicles including reentry and airbreathing cruise vehicles. This includes complex three-dimensional forebody laminar simulations, turbulent shock-train for internal aerodynamics, and axisymmetric triconic cases. A demonstration on a full cruise vehicle, with a modeled scramjet engine, is then conducted and presented as an illustration of future possible use of the tool.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/10\/HISST2025_74_paper.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Mathieu LUGRIN, Baptiste ISNARD, Bruno MAUGARS, Cedric CONTENT<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: HiSST-2025-074<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,3367,3361],"tags":[442,440,3704],"class_list":["post-23059","post","type-post","status-publish","format-standard","hentry","category-events","category-high-speed-aerodynamics-and-aerothermodynamics-with-application-to-hypersonic-regimes","category-1-hisst-2025","tag-cfd","tag-hypersonic","tag-mesh-adaptation-2","category-993","category-3367","category-3361","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/23059","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=23059"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/23059\/revisions"}],"predecessor-version":[{"id":23061,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/23059\/revisions\/23061"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=23059"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=23059"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=23059"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}