{"id":16413,"date":"2024-04-24T13:33:51","date_gmt":"2024-04-24T13:33:51","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16413"},"modified":"2024-04-24T13:33:51","modified_gmt":"2024-04-24T13:33:51","slug":"high-heat-flux-testing-of-yttria-stabilized-zirconia-coatings-on-titanium","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/24\/high-heat-flux-testing-of-yttria-stabilized-zirconia-coatings-on-titanium\/","title":{"rendered":"High Heat Flux Testing of Yttria-stabilized Zirconia Coatings on Titanium"},"content":{"rendered":"\n<p><strong>Philipp Nieke, Steve Matthews, Nicholas J. Rattenbury, John E. Cater<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-412<\/strong><\/p>\n\n\n\n<p>Thermal barrier coatings are attractive thermal protection materials for hypersonic vehicles. We study<br>Yttria-stabilized-Zirconia coatings on pure Titanium and their performance under heat fluxes relevant<br>to hypersonic flight. Coatings were successfully manufactured by air plasma spray, each consisting<br>of a bond coat and a top coat, made from NiCrAlY alloy powder and Yttria-stabilized Zirconia powder,<br>respectively. The predicted peak heat flux of a hypersonic vehicle is simulated with the help of a custom-<br>built Oxy-Acetylene torch apparatus. Coated and uncoated Titanium substrates are subjected to a cold<br>wall heat flux of 900 kW\/m2 for 60 s. Yttria-stabilized-Zirconia coated specimens show no external<br>damage, and for some, performance metrics are about one third higher than for uncoated samples.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/04\/HiSST-2022-412.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Philipp Nieke, Steve Matthews, Nicholas J. Rattenbury, John E. Cater<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-412<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[1006],"tags":[1318,1320,1322,1319,1321],"class_list":["post-16413","post","type-post","status-publish","format-standard","hentry","category-hisst-2022","tag-air-plasma-spray","tag-oxy-acetylene-burner-testing","tag-thermal-barrier-coatings","tag-titanium","tag-yttria-stabilized-zirconia","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16413","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=16413"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16413\/revisions"}],"predecessor-version":[{"id":16415,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16413\/revisions\/16415"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16413"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16413"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16413"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}