{"id":17140,"date":"2024-06-05T13:27:25","date_gmt":"2024-06-05T13:27:25","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=17140"},"modified":"2025-09-21T14:04:53","modified_gmt":"2025-09-21T14:04:53","slug":"numerical-solution-of-transpiration-cooling-method-in-hypersonic-laminar-flow-using-the-kinetic-theory-model","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/05\/numerical-solution-of-transpiration-cooling-method-in-hypersonic-laminar-flow-using-the-kinetic-theory-model\/","title":{"rendered":"Numerical Solution of Transpiration Cooling Method in Hypersonic Laminar Flow using the Kinetic Theory Model"},"content":{"rendered":"\n<p><strong>Davoud HOSSEINZADEH, Esmail LAKZIAN, Hassan Saad LFIT, Ikhyun KIM<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: 10.82241\/ceas-hisst-2024-238<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2024-238<\/strong><\/p>\n\n\n\n<p>Transpiration cooling method is proved to be an effective cooling method to diminish the heat flux on the special area of the surfaces of the high-speed vehicles. The cooling process is investigated using nitrogen gas as the coolant and air as the main flow. This study presents a novel approach, as transpiration cooling in hypersonic laminar flow has not been previously simulated through kinetic theory. The kinetic theory is used to compute properties of the mixture of the coolant and main flow. Nitrogen gas and Air are used as coolant and main flow, respectively. Details will be elaborated in the session.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/06\/HiSST-2024-238.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Davoud HOSSEINZADEH, Esmail LAKZIAN, Hassan Saad LFIT, Ikhyun KIM<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82241\/ceas-hisst-2024-238<\/p>\n<p>Conference number: HiSST-2024-238<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1407,1416],"tags":[1774,1578,1773],"class_list":["post-17140","post","type-post","status-publish","format-standard","hentry","category-events","category-11-hisst-2024","category-thermal-and-energy-management","tag-hypersonic-laminar-flow","tag-porous-media","tag-transpiration-cooling-method","category-993","category-1407","category-1416","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17140","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=17140"}],"version-history":[{"count":4,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17140\/revisions"}],"predecessor-version":[{"id":21246,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17140\/revisions\/21246"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=17140"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=17140"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=17140"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}