{"id":16425,"date":"2024-04-25T09:58:57","date_gmt":"2024-04-25T09:58:57","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16425"},"modified":"2024-04-25T09:58:58","modified_gmt":"2024-04-25T09:58:58","slug":"numerical-investigation-of-leading-edge-bluntness-effect-on-scramjetinlet-at-mach-6","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/04\/25\/numerical-investigation-of-leading-edge-bluntness-effect-on-scramjetinlet-at-mach-6\/","title":{"rendered":"Numerical investigation of leading-edge bluntness effect on Scramjetinlet at Mach 6"},"content":{"rendered":"\n<p><strong>Talluri Vamsi Krishna, Saranyamol VS, Desikan SLN, Mohammed Ibrahim Sugarno<\/strong><\/p>\n\n\n\n<p><strong>DOI Number XXX-YYY-ZZZ<\/strong><\/p>\n\n\n\n<p><strong>Conference Number HiSST-2022-416<\/strong><\/p>\n\n\n\n<p>The leading-edge bluntness plays an important parameter in influencing separation and shock boundary<br>layer interactions. Current work is to investigate the effect of the sharp and blunt leading edges at<br>Mach 6 to understand the wall heat fluxes and flow characteristics of a scramjet intake. A detailed two<br>-dimensional computational study carried out using commercially available Ansys Fluent software. Three<br>different nose tip radii of 0, 0.5 &amp; 1.0 mm analyzed for ramp and cowl individually. Radius of 0.5 mm<br>shows no significant change in the flow field for the all the configurations simulated. When the tip<br>radius increased to 1.0 mm, peak pressure loads were increased marginally and peak heat transfer to<br>the wall decreased significantly for all the configurations tested. This study provided better insights into<br>understanding nose tip bluntness effect on ramp, cowl and combination of both with respect to shock<br>boundary layer intractions.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/04\/HiSST-2022-416.pdf\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Talluri Vamsi Krishna, Saranyamol VS, Desikan SLN, Mohammed Ibrahim Sugarno<\/b><\/p>\n<p>DOI Number XXX-YYY-ZZZ<\/p>\n<p>Conference Number HiSST-2022-416<\/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":[539,621,614,924,1229],"class_list":["post-16425","post","type-post","status-publish","format-standard","hentry","category-hisst-2022","tag-boundary-layer","tag-inlet","tag-scramjet","tag-separation-bubble","tag-swbli","category-1006","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16425","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=16425"}],"version-history":[{"count":1,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16425\/revisions"}],"predecessor-version":[{"id":16427,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16425\/revisions\/16427"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16425"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16425"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16425"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}