{"id":513,"date":"2025-03-02T14:09:22","date_gmt":"2025-03-02T14:09:22","guid":{"rendered":"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/?page_id=513"},"modified":"2025-07-24T05:48:17","modified_gmt":"2025-07-24T05:48:17","slug":"modeling-of-rotating-detonation-engine","status":"publish","type":"page","link":"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/","title":{"rendered":"Study of Rotating Detonation Engine Combustor"},"content":{"rendered":"\n<h3 class=\"wp-block-heading\">Summary<\/h3>\n\n\n\n<p>The focus of this research effort is to perform computational modeling and analysis of reacting flow physics within a rotating detonation engine (RDE) combustor. We consider the AFRL RDE combustor configuration at the global equivalence ratio, \u03d5 = 1, which exhibits the presence of a single detonation front propagating in a cyclic manner in the annular combustion chamber. After establishing the single wave mode, when the mass flow rates of fuel and oxidizer are altered ensuring the same value of \u03d5, the wave mode transition occurs from a sustained single detonation wave structure to a double co-rotating detonation wave structure. We focus on computational investigation of the transition phenomenon.<\/p>\n\n\n<div class=\"wp-block-image is-style-book-style\">\n<figure class=\"aligncenter size-large is-resized\"><img loading=\"lazy\" decoding=\"async\" width=\"1024\" height=\"806\" src=\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/03\/RDE-1024x806.jpg\" alt=\"\" class=\"wp-image-524\" style=\"width:534px;height:auto\" srcset=\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/03\/RDE-1024x806.jpg 1024w, https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/03\/RDE-768x605.jpg 768w, https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/03\/RDE-1536x1210.jpg 1536w, https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/03\/RDE-2048x1613.jpg 2048w, https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/03\/RDE-580x457.jpg 580w, https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/03\/RDE-610x480.jpg 610w\" sizes=\"auto, (max-width: 1024px) 100vw, 1024px\" \/><\/figure><\/div>\n\n\n<h3 class=\"wp-block-heading\">Support<\/h3>\n\n\n\n<p>N\/A<\/p>\n\n\n\n<h3 class=\"wp-block-heading\">Test Case<\/h3>\n\n\n\n<p>AFRL RDE Combustor<\/p>\n\n\n\n<h3 class=\"wp-block-heading\">Computational Approaches<\/h3>\n\n\n\n<p>The simulations are being performed by Dr. Hasti&#8217;s group using  the commercial <a href=\"https:\/\/convergecfd.com\/\">CONVERGE CFD Software<\/a>. The comprehensive analysis is performed using statistical, spectral, and modal analysis tools developed within the FCM research group. These analysis tools are developed using Python-based scripting. A particular focus is on the understanding of the wave mode transition phenomenon that is observed in experiments when the inflow conditions are modified while keeping the same equivalence ratio (\u03d5 = 1).<\/p>\n\n\n\n<h3 class=\"wp-block-heading\">Publications<\/h3>\n\n\n\n<ol class=\"wp-block-list\">\n<li>V. R. Hasti and R. Ranjan, &#8220;Numerical Investigation of Wave Dynamics During Mode Transition in a Hydrogen-Fueled Rotating Detonation Engine Combustor&#8221;, Publication  ASME Journal of Thermal Science and Engineering Applications, <em>Accepted<\/em>, 2025.<\/li>\n\n\n\n<li>V. R. Hasti, J. Pratt, and R. Ranjan, &#8220;<a href=\"https:\/\/arc.aiaa.org\/doi\/abs\/10.2514\/6.2025-0402\">Dynamically Dominant Flow Features During Wave Mode Transition in a Rotating Detonation Engine Combusto<\/a>r&#8221;, AIAA-2025-0402, 2025.<\/li>\n\n\n\n<li>V. R. Hasti, S. Thompson, and R. Ranjan, &#8220;Analysis of Mixing Efficiency and Detonation Wave Structure during Wave Splitting in a Hydrogen-Fueled Rotating Detonation Engine Combustor&#8221;, 77th Annual Meeting of the Division of Fluid Dynamics, November 24\u201326, 2024, Salt Lake City, Utah.<\/li>\n\n\n\n<li>V. R. Hasti and R. Ranjan, &#8220;<a href=\"https:\/\/doi.org\/10.1115\/IMECE2024-145858\">Numerical Investigation of Wave Dynamics During Mode Transition in a Hydrogen-Fueled Rotating Detonation Engine Combusto<\/a>r&#8221;, ASME IMECE2024-145858, V009T11A034, 2024.<\/li>\n<\/ol>\n","protected":false},"excerpt":{"rendered":"<p>Summary The focus of this research effort is to perform computational modeling and analysis of reacting flow physics within a rotating detonation engine (RDE) combustor. We consider the AFRL RDE combustor configuration at the global equivalence ratio, \u03d5 = 1, which exhibits the presence of a single detonation front propagating in a cyclic manner in&hellip; <\/p>\n<p class=\"more-link-wrap\"><span><a class=\"more-link button text\" href=\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/\"><span>Continue Reading <\/span><\/a><\/span><\/p>\n","protected":false},"author":1459,"featured_media":516,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_genesis_hide_title":false,"_genesis_hide_breadcrumbs":false,"_genesis_hide_singular_image":false,"_genesis_hide_footer_widgets":false,"_genesis_custom_body_class":"","_genesis_custom_post_class":"","_genesis_layout":"","footnotes":""},"class_list":{"0":"post-513","1":"page","2":"type-page","3":"status-publish","4":"has-post-thumbnail","6":"entry"},"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v25.5 - https:\/\/yoast.com\/wordpress\/plugins\/seo\/ -->\n<title>Study of Rotating Detonation Engine Combustor - Reetesh Ranjan Archive<\/title>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/\" \/>\n<meta property=\"og:locale\" content=\"en_US\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Study of Rotating Detonation Engine Combustor - Reetesh Ranjan Archive\" \/>\n<meta property=\"og:description\" content=\"Summary The focus of this research effort is to perform computational modeling and analysis of reacting flow physics within a rotating detonation engine (RDE) combustor. We consider the AFRL RDE combustor configuration at the global equivalence ratio, \u03d5 = 1, which exhibits the presence of a single detonation front propagating in a cyclic manner in&hellip; Continue Reading\" \/>\n<meta property=\"og:url\" content=\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/\" \/>\n<meta property=\"og:site_name\" content=\"Reetesh Ranjan Archive\" \/>\n<meta property=\"article:modified_time\" content=\"2025-07-24T05:48:17+00:00\" \/>\n<meta name=\"twitter:card\" content=\"summary_large_image\" \/>\n<meta name=\"twitter:label1\" content=\"Est. reading time\" \/>\n\t<meta name=\"twitter:data1\" content=\"2 minutes\" \/>\n<script type=\"application\/ld+json\" class=\"yoast-schema-graph\">{\"@context\":\"https:\/\/schema.org\",\"@graph\":[{\"@type\":\"WebPage\",\"@id\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/\",\"url\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/\",\"name\":\"Study of Rotating Detonation Engine Combustor - Reetesh Ranjan Archive\",\"isPartOf\":{\"@id\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/#website\"},\"primaryImageOfPage\":{\"@id\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/#primaryimage\"},\"image\":{\"@id\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/#primaryimage\"},\"thumbnailUrl\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/01\/pres_evolve-pdf.jpg\",\"datePublished\":\"2025-03-02T14:09:22+00:00\",\"dateModified\":\"2025-07-24T05:48:17+00:00\",\"breadcrumb\":{\"@id\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/#breadcrumb\"},\"inLanguage\":\"en-US\",\"potentialAction\":[{\"@type\":\"ReadAction\",\"target\":[\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/\"]}]},{\"@type\":\"ImageObject\",\"inLanguage\":\"en-US\",\"@id\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/#primaryimage\",\"url\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/01\/pres_evolve-pdf.jpg\",\"contentUrl\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/files\/2025\/01\/pres_evolve-pdf.jpg\"},{\"@type\":\"BreadcrumbList\",\"@id\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/#breadcrumb\",\"itemListElement\":[{\"@type\":\"ListItem\",\"position\":1,\"name\":\"Home\",\"item\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/\"},{\"@type\":\"ListItem\",\"position\":2,\"name\":\"Study of Rotating Detonation Engine Combustor\"}]},{\"@type\":\"WebSite\",\"@id\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/#website\",\"url\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/\",\"name\":\"Reetesh Ranjan Archive\",\"description\":\"Mechanical Engineering\",\"potentialAction\":[{\"@type\":\"SearchAction\",\"target\":{\"@type\":\"EntryPoint\",\"urlTemplate\":\"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/?s={search_term_string}\"},\"query-input\":{\"@type\":\"PropertyValueSpecification\",\"valueRequired\":true,\"valueName\":\"search_term_string\"}}],\"inLanguage\":\"en-US\"}]}<\/script>\n<!-- \/ Yoast SEO plugin. -->","yoast_head_json":{"title":"Study of Rotating Detonation Engine Combustor - Reetesh Ranjan Archive","robots":{"index":"index","follow":"follow","max-snippet":"max-snippet:-1","max-image-preview":"max-image-preview:large","max-video-preview":"max-video-preview:-1"},"canonical":"https:\/\/blogarchive.utc.edu\/reetesh-ranjan\/modeling-of-rotating-detonation-engine\/","og_locale":"en_US","og_type":"article","og_title":"Study of Rotating Detonation Engine Combustor - Reetesh Ranjan Archive","og_description":"Summary The focus of this research effort is to perform computational modeling and analysis of reacting flow physics within a rotating detonation engine (RDE) combustor. 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