{"id":16449,"date":"2024-04-25T10:31:32","date_gmt":"2024-04-25T10:31:32","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16449"},"modified":"2024-04-25T10:31:33","modified_gmt":"2024-04-25T10:31:33","slug":"numerical-investigation-of-different-ramp-models-and-length-on-shockwave-boundary-layer-interactions","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/25\/numerical-investigation-of-different-ramp-models-and-length-on-shockwave-boundary-layer-interactions\/","title":{"rendered":"Numerical Investigation of Different Ramp Models and Length on ShockWave Boundary Layer Interactions"},"content":{"rendered":"\n<p><strong>Fatmanur Aleyna \u00d6ZCAN, Muhammed Osama BALKHI, Ahmet Selim DURNA<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-429<\/strong><\/p>\n\n\n\n<p>Shock-wave boundary layer interaction is therefore a spectacle commonly associated with aerospace<br>devices when a shock wave meets a boundary layer in high-speed flows. In this study, the effect of<br>different ramp lengths at three different ramp angles of 24\u00ba, 33\u00ba, and 50\u00ba, respectively, at M=2.52 will<br>be examined. Investigations were performed with a commercial Computational Fluid Dynamics software<br>based on two different ramp angle geometries with Schlieren images. The results obtained are<br>compatible with the experimental results. The separation shock&#8217;s angle is independent of ramp angle<br>and length. Separation width increases with ramp angle and length. The separation shock&#8217;s strength<br>increases with ramp angle, however reattachment shock&#8217;s strength almost stays constant.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/04\/HiSST-2022-429.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Fatmanur Aleyna \u00d6ZCAN, Muhammed Osama BALKHI, Ahmet Selim DURNA<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-429<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1006],"tags":[1357,1355,1356],"class_list":["post-16449","post","type-post","status-publish","format-standard","hentry","category-events","category-hisst-2022","tag-compression-ramp","tag-ramp-length-effect","tag-shock-wave-boundary-layer-interaction","category-993","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16449","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=16449"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16449\/revisions"}],"predecessor-version":[{"id":16451,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16449\/revisions\/16451"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16449"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16449"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16449"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}