{"id":16096,"date":"2024-04-12T09:11:34","date_gmt":"2024-04-12T09:11:34","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16096"},"modified":"2024-04-12T09:11:35","modified_gmt":"2024-04-12T09:11:35","slug":"development-of-performance-test-rig-for-heat-exchanger-of-supersonic-regenerative-cooling-combustor","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/development-of-performance-test-rig-for-heat-exchanger-of-supersonic-regenerative-cooling-combustor\/","title":{"rendered":"Development of Performance Test Rig for Heat Exchanger of Supersonic Regenerative Cooling Combustor"},"content":{"rendered":"\n<p><strong>Kyungjae LEE , Inyoung YANG , Yangji LEE , Sanghoon LEE<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-13<\/strong><\/p>\n\n\n\n<p>A performance test rig for heat exchanger of a supersonic regenerative cooling combustor was<br>developed in Korea Aerospace Research Institute. The 500 hp compressor was used to supply air of<br>more than 2 bar and the air was heated through two electric air heaters, which had a capacity of 300<br>kW and 400 kW, respectively. Max. air flow is about 0.7 kg\/s and max. air temperature is about 600<br>\u2103. The heated air is accelerated up to Mach 2 with supersonic nozzle. A preliminary performance test<br>was carried out with heat exchanger of a supersonic regenerative cooling combustor model at Mach 2<br>air flow and air temperature was varied from 300 to 500 \u2103. And room temperature water was supplied<br>as a fuel and coolant of heat exchanger instead of real fuel for safety reason.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-13.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-13.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Kyungjae LEE , Inyoung YANG , Yangji LEE , Sanghoon LEE<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-13<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1006,1014],"tags":[1032,1031,856],"class_list":["post-16096","post","type-post","status-publish","format-standard","hentry","category-events","category-hisst-2022","category-testing-and-evaluation-hisst-2022","tag-heat-exchanger","tag-regenerative-cooling-test-rig","tag-supersonic-combustor","category-993","category-1006","category-1014","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16096","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=16096"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16096\/revisions"}],"predecessor-version":[{"id":16097,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16096\/revisions\/16097"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16096"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16096"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16096"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}