{"id":23247,"date":"2025-10-26T11:53:08","date_gmt":"2025-10-26T11:53:08","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=23247"},"modified":"2025-10-26T11:53:09","modified_gmt":"2025-10-26T11:53:09","slug":"a-quasi-neutral-approach-to-simulate-plasma-assisted-combustion-in-supersonic-flow","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2025\/10\/26\/a-quasi-neutral-approach-to-simulate-plasma-assisted-combustion-in-supersonic-flow\/","title":{"rendered":"A quasi neutral approach to simulate plasma-assisted combustion in supersonic flow."},"content":{"rendered":"\n<p><strong>Julien LABAUNE, Ancelin ROCAMORA, Aymeric BOURLET, Christophe LAUX, Fabien THOLIN<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2025-027<\/strong><\/p>\n\n\n\n<p>The primary objective of this study is to establish a numerical strategy for simulating a supersonic combustion chamber where plasma is utilized to ignite combustion. Following a description of the methodology based on the quasi-neutrality hypothesis for simulating the plasma, simulations are conducted in non-reactive and reactive conditions. Qualitative comparisons are made with an experiment for non-reactive case. A second simulation aims to predict outcomes for future experimental investigations.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2025\/10\/HISST2025_27_paper.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Julien LABAUNE, Ancelin ROCAMORA, Aymeric BOURLET, Christophe LAUX, Fabien THOLIN<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: HiSST-2025-027<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,3361,3363],"tags":[3735,744],"class_list":["post-23247","post","type-post","status-publish","format-standard","hentry","category-events","category-1-hisst-2025","category-propulsion-systems-components","tag-plasma-assisted","tag-supersonic-flow","category-993","category-3361","category-3363","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/23247","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=23247"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/23247\/revisions"}],"predecessor-version":[{"id":23251,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/23247\/revisions\/23251"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=23247"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=23247"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=23247"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}