{"id":16422,"date":"2024-04-25T09:55:53","date_gmt":"2024-04-25T09:55:53","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16422"},"modified":"2024-04-25T09:55:53","modified_gmt":"2024-04-25T09:55:53","slug":"investigation-of-shock-patterns-around-a-double-wedge-for-hypersonicflows-in-thermochemical-non-equilibrium","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/25\/investigation-of-shock-patterns-around-a-double-wedge-for-hypersonicflows-in-thermochemical-non-equilibrium\/","title":{"rendered":"Investigation of Shock Patterns around a Double-Wedge for HypersonicFlows in Thermochemical Non-Equilibrium"},"content":{"rendered":"\n<p><strong>Maxime Lalande, Chay W. C. Atkins, Ralf Deiterding<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-415<\/strong><\/p>\n\n\n\n<p>Numerical simulations of hypersonic viscous flow in thermochemical non-equilibrium over a double<br>wedge with high Mach and high enthalpy inflow conditions are performed to investigate shock pat-<br>tern transition. First, simulations for varying second wedge angle are conducted in order to classify the<br>shock patterns. Then, the effects of the thermochemistry on shock pattern transition are investigated<br>by comparing simulations with air, nitrogen and an ideal gas flow. The highlighted effects of the second<br>wedge angle, time and thermochemistry modelling on pattern transition are supported by a shock polar<br>analysis. Finally, quantitative transition criteria are provided to summarise the influence of these three<br>parameters.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/04\/HiSST-2022-415.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Maxime Lalande, Chay W. C. Atkins, Ralf Deiterding<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-415<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[1006],"tags":[492,1330,1331],"class_list":["post-16422","post","type-post","status-publish","format-standard","hentry","category-hisst-2022","tag-numerical-simulation","tag-shock-patterns","tag-shock-boundary-layer-interaction","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16422","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=16422"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16422\/revisions"}],"predecessor-version":[{"id":16424,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16422\/revisions\/16424"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16422"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16422"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16422"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}