{"id":312,"date":"2017-08-02T07:05:31","date_gmt":"2017-08-02T12:05:31","guid":{"rendered":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/?page_id=312"},"modified":"2026-03-23T14:24:52","modified_gmt":"2026-03-23T18:24:52","slug":"supersonic-wind-tunnel","status":"publish","type":"page","link":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/facilities\/supersonic-wind-tunnel\/","title":{"rendered":"Supersonic Wind Tunnel"},"content":{"rendered":"<p>This blow down wind tunnel currently has a fixed nozzle block designed to run at Mach 1.44.\u00a0 The test section, which is 3 X 4 inches, can have optical access from all sides and is currently being used for the studies on control of supersonic flow over open cavities and the interaction of incident shock waves with vibratory metamaterials.\u00a0 \u00a0Air to the wind tunnel is supplied by a Sullair Compressor, passed through a desiccant dryer and stored in two large storage tanks.<\/p>\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" decoding=\"async\" width=\"1024\" height=\"263\" src=\"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-content\/uploads\/sites\/723\/2026\/01\/sswt-1024x263.jpg\" alt=\"Picture of Supersonic Wind tunnel\" class=\"wp-image-1137\" srcset=\"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-content\/uploads\/sites\/723\/2026\/01\/sswt-1024x263.jpg 1024w, https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-content\/uploads\/sites\/723\/2026\/01\/sswt-300x77.jpg 300w, https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-content\/uploads\/sites\/723\/2026\/01\/sswt-768x197.jpg 768w, https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-content\/uploads\/sites\/723\/2026\/01\/sswt.jpg 1449w\" sizes=\"auto, (max-width: 1024px) 100vw, 1024px\" \/><\/figure>\n","protected":false},"excerpt":{"rendered":"<p>This blow down wind tunnel currently has a fixed nozzle block designed to run at Mach 1.44.\u00a0 The test section, which is 3 X 4 inches, can have optical access from all sides and is currently being used for the studies on control of supersonic flow over open cavities and the interaction of incident shock [&hellip;]<\/p>\n","protected":false},"author":76,"featured_media":0,"parent":65,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"page-templates\/page-sidebar-none.php","meta":{"_acf_changed":false,"inline_featured_image":false,"featured_post":"","footnotes":"","_links_to":"","_links_to_target":""},"class_list":["post-312","page","type-page","status-publish","hentry"],"acf":[],"_links":{"self":[{"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/pages\/312","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/users\/76"}],"replies":[{"embeddable":true,"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/comments?post=312"}],"version-history":[{"count":4,"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/pages\/312\/revisions"}],"predecessor-version":[{"id":1407,"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/pages\/312\/revisions\/1407"}],"up":[{"embeddable":true,"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/pages\/65"}],"wp:attachment":[{"href":"https:\/\/faculty.eng.ufl.edu\/unsteady-fluid-dynamics-group\/wp-json\/wp\/v2\/media?parent=312"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}