{"id":16760,"date":"2024-05-10T10:19:07","date_gmt":"2024-05-10T10:19:07","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=16760"},"modified":"2025-09-16T09:57:24","modified_gmt":"2025-09-16T09:57:24","slug":"analytical-model-of-curved-shock-inverse-mach-reflection","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/05\/10\/analytical-model-of-curved-shock-inverse-mach-reflection\/","title":{"rendered":"Analytical Model of Curved-shock Inverse Mach Reflection"},"content":{"rendered":"\n<p><strong>Chongguang SHI, Rongguang SU, Tao ZHANG, Chengxiang ZHU, Yancheng YOU<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: <\/strong><a href=\"https:\/\/doi.org\/10.1063\/5.0139784\" target=\"_blank\" rel=\"noreferrer noopener\">10.1063\/5.0139784<\/a><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2024-069<\/strong><\/p>\n\n\n\n<p>Mach reflection (MR) is an essential component in the development of the shock theory, as well as the transition between regular reflection (RR) and Mach reflection. The hysteresis of Curved-shock reflection (CR) is not yet adequately understood due to the rotational complexity behind curved shocks. Here, an inverse Mach reflection (IMR), which is possible only in truly unsteady oblique-shock reflection (OR) transition, is found possible to be stable in CR. An analytical model for predicting the stable curved-shock IMR (CIMR) structure is established. Predictions of the Mach stem height and shock structure based on the model exhibit a great agreement with the numerical results. It is found that the compressive waves play a key role in generating the stable CIMR structure.<\/p>\n\n\n\n<p><a href=\"https:\/\/pubs.aip.org\/aip\/pof\/article\/35\/3\/031702\/2881620\/Analytical-model-for-curved-shock-Mach-reflection\">Read the full paper here<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Chongguang SHI, Rongguang SU, Tao ZHANG, Chengxiang ZHU, Yancheng YOU<\/b><\/p>\n<p>DOI Number: 10.1063\/5.0139784<\/p>\n<p>Conference number: HiSST-2024-069<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1407,1411],"tags":[1504,1503,1506,1505],"class_list":["post-16760","post","type-post","status-publish","format-standard","hentry","category-events","category-11-hisst-2024","category-hypersonic-fundamentals-and-history-11-hisst-2024","tag-curved-shock","tag-inverse-mach-reflection","tag-mach-stem","tag-shock-reflection","category-993","category-1407","category-1411","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16760","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=16760"}],"version-history":[{"count":2,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16760\/revisions"}],"predecessor-version":[{"id":21010,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/16760\/revisions\/21010"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=16760"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=16760"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=16760"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}