{"id":13449,"date":"2023-10-17T14:31:40","date_gmt":"2023-10-17T14:31:40","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13449"},"modified":"2024-05-03T14:31:27","modified_gmt":"2024-05-03T14:31:27","slug":"numerical-solution-of-the-problem-of-flow-and-heat-exchange-in-model-chambers-of-combustion-of-high-speed-direct-air-reactor-engines-on-hydrogen-fuel","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/17\/numerical-solution-of-the-problem-of-flow-and-heat-exchange-in-model-chambers-of-combustion-of-high-speed-direct-air-reactor-engines-on-hydrogen-fuel\/","title":{"rendered":"NUMERICAL SOLUTION OF THE PROBLEM OF FLOW AND HEAT EXCHANGE IN MODEL CHAMBERS OF COMBUSTION OF HIGH-SPEED DIRECT AIR-REACTOR ENGINES ON HYDROGEN FUEL"},"content":{"rendered":"\n<p><strong>Serpinsky O. S., Frantsuzov M.S<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST 2018_3130978<\/strong><\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p>The development of technologies and materials used for high-speed ramjets makes it possible to significantly increase the life of the engine. In this regard, an obligatory element of the combustion chamber design is an active cooling system that provides acceptable values of the temperature of the fire walls. Numerical simulation of the conjugate heat exchange problem allows to predict the thermal state of the walls of the combustion chamber and to reveal physical features<\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_3130978.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_3130978.pdf\">Read the full paper &gt;<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Serpinsky O. S., Frantsuzov M.S<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST 2018_3130978<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[185,994,257,1001,1003],"tags":[434],"class_list":["post-13449","post","type-post","status-publish","format-standard","hentry","category-papers-flight-mechanics","category-hisst-2018","category-hypersonic-flight-dynamics","category-propulsion-systems-and-components","category-thermal-and-energy-management-systems","tag-hisst-2018","category-185","category-994","category-257","category-1001","category-1003","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13449","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=13449"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13449\/revisions"}],"predecessor-version":[{"id":16554,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13449\/revisions\/16554"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13449"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13449"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13449"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}