{"id":16262,"date":"2024-04-12T13:35:17","date_gmt":"2024-04-12T13:35:17","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16262"},"modified":"2024-04-12T13:35:18","modified_gmt":"2024-04-12T13:35:18","slug":"shock-dominated-flow-control-by-patterned-plasmas","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/12\/shock-dominated-flow-control-by-patterned-plasmas\/","title":{"rendered":"Shock-Dominated Flow Control by Patterned Plasmas"},"content":{"rendered":"\n<p><strong>Philip Andrews, Philip Lax, Sergey B Leonov<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-393<\/strong><\/p>\n\n\n\n<p>The results of an experimental study of shock-dominated flow controlled by a patterned electrical<br>discharge are discussed. A solid wedge shock wave (SW) generator was installed in test section of M=4<br>wind tunnel. The Q-DC filamentary electrical discharge was arranged on the opposite wall so that the<br>SW originating from the wedge impinged the area partially occupied with the plasma filaments arranged<br>in a flow-wise direction with either a row of three filaments or only a single central filament. As a result<br>of the SW-plasma interaction, the flowfield was significantly modified over the test section, including<br>an upstream shift of the shock train. The details of the plasma-SW interaction, including the transitional<br>effects, are explored with wall pressure measurements, schlieren imaging and Mie scattering<br>visualization. The physics of the flow control effect is discussed.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-393.pdf\" data-type=\"link\" data-id=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2023\/10\/HiSST-2022-393.pdf\">Read the full paper > <\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Philip Andrews, Philip Lax, Sergey B Leonov<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-393<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1008,1006],"tags":[1227,1231,1228,1230,1229],"class_list":["post-16262","post","type-post","status-publish","format-standard","hentry","category-events","category-high-speed-aerodynamics-and-aerothermodynamics-hisst-2022","category-hisst-2022","tag-impinging-sw","tag-mie-scattering","tag-q-dc-plasma","tag-shock-train-control","tag-swbli","category-993","category-1008","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16262","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=16262"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16262\/revisions"}],"predecessor-version":[{"id":16263,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16262\/revisions\/16263"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16262"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16262"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16262"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}