{"id":16250,"date":"2024-04-12T13:20:52","date_gmt":"2024-04-12T13:20:52","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16250"},"modified":"2024-04-12T13:20:53","modified_gmt":"2024-04-12T13:20:53","slug":"direct-numerical-simulation-of-the-multispecies-hypersonic-boundary-layers-effect-of-gas-surface-interaction-on-wall-heating","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/direct-numerical-simulation-of-the-multispecies-hypersonic-boundary-layers-effect-of-gas-surface-interaction-on-wall-heating\/","title":{"rendered":"Direct numerical simulation of the multispecies hypersonic boundary layers: effect of gas-surface interaction on wall heating\u00a0"},"content":{"rendered":"\n<p><strong>Mona Karimi &amp; Christian Stemmer<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-377<\/strong><\/p>\n\n\n\n<p>Planetary entry environment of hypersonic vehicles presents the extreme effects of high-temperature<br>real-gas. Aeroshell of spacecraft heat shields are made of ablative materials in order to survive such<br>high-energy environments. Ablation can impact surface heating via injecting pyrolysis gas into the<br>boundary layer, thus prompt a strong interaction between the surface ablative materials and the boundary layer flow. By means of direction numerical simulation, the current study examines the effect of<br>blowing at the wall on the aeroheating within the boundary layer subject to the thermochemical effects<br>of vibrational excitation and dissociation of air mixture in hypersonic chemically reacting flows.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-377.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-377.pdf\">Read the full paper ><\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Mona Karimi &#038; Christian Stemmer<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-377<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1008,1006],"tags":[872,1221,1223,1222],"class_list":["post-16250","post","type-post","status-publish","format-standard","hentry","category-events","category-high-speed-aerodynamics-and-aerothermodynamics-hisst-2022","category-hisst-2022","tag-ablation","tag-aeroheating","tag-blowing-effect","tag-hypersonic-boundary-layers","category-993","category-1008","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16250","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\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=16250"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16250\/revisions"}],"predecessor-version":[{"id":16251,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16250\/revisions\/16251"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16250"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16250"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16250"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}