{"id":13493,"date":"2023-10-26T18:43:52","date_gmt":"2023-10-26T18:43:52","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=13493"},"modified":"2024-05-03T14:21:55","modified_gmt":"2024-05-03T14:21:55","slug":"experimental-investigation-of-thermo-barrier-coating-based-on-zirconium-dioxide","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2023\/10\/26\/experimental-investigation-of-thermo-barrier-coating-based-on-zirconium-dioxide\/","title":{"rendered":"Experimental Investigation of Thermo-barrier Coating Based on Zirconium Dioxide"},"content":{"rendered":"\n<p><strong>A. Shardin&nbsp; , K. Zhirikhin, S. Kazhichkin, A. Nikulenko, V. Talyzin, E. Dmitriev, A. Sysoev, D. Somov, Yu. Tarasenko<\/strong><\/p>\n\n\n\n<p> <\/p>\n\n\n\n<div style=\"height:50px\" aria-hidden=\"true\" class=\"wp-block-spacer\"><\/div>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST 2018_19101571<\/strong><\/p>\n\n\n\n<p>One of the main problems in design and manufacture of a high-speed civil vehicles, an aerodynamic models or an experimental facility equipment, subjected to withstand a high-temperature loads, is a combination of optimal choice of construction materials and methods of their protection against the destructive influence of high temperatures. Because of a maximum melting point of most applicable materials usually remains insufficient for operation in a high temperature zones, such as a nose part, wing or tail leading edges of a vehicle or aerodynamic model, arises the necessity of usage of a thermobarrier heat-resistant coating on the edges or other outer curvilinear surfaces of the constructions subjected to the high temperature. The thermo-barrier coating is selected in terms of its structural compatibility with used materials, required protective and mechanical characteristics. To approve the applied thermo-barrier protective coating method, a series of experimental investigation at a high temperature research facility with a samples made from same material as the reference construction and covered with the thermo-barrier coating are provided<\/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_19101571.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/hisst-2018_19101571.pdf\">Read the full paper &gt; <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>A. Shardin\u00a0 , K. Zhirikhin, S. Kazhichkin, A. Nikulenko, V. Talyzin, E. Dmitriev, A. Sysoev, D. Somov, Yu. Tarasenko<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ <\/p>\n<p>Conference Number HiSST 2018_19101571<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[274,994,82,999,397,296,337],"tags":[836,434,837,838],"class_list":["post-13493","post","type-post","status-publish","format-standard","hentry","category-aircraft-design-and-materials","category-hisst-2018","category-papers-materials-and-structures","category-materials-and-structures-hisst-2018","category-thermal-environmental-control-systems","category-thermal-protection-systems","category-thermal-protection-systems-space-materials-and-structures","tag-coating","tag-hisst-2018","tag-thermo-barrier","tag-zirconium-dioxide","category-274","category-994","category-82","category-999","category-397","category-296","category-337","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13493","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=13493"}],"version-history":[{"count":3,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13493\/revisions"}],"predecessor-version":[{"id":16537,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/13493\/revisions\/16537"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=13493"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=13493"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=13493"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}