{"id":17056,"date":"2024-06-03T14:12:53","date_gmt":"2024-06-03T14:12:53","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=17056"},"modified":"2025-09-15T12:56:24","modified_gmt":"2025-09-15T12:56:24","slug":"ignition-delay-study-of-liquid-nano-fuels-for-application-in-pulse-detonation-engines-using-a-shock-tube","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/03\/ignition-delay-study-of-liquid-nano-fuels-for-application-in-pulse-detonation-engines-using-a-shock-tube\/","title":{"rendered":"Ignition Delay Study of Liquid Nano-fuels for Application in Pulse Detonation Engines using a Shock Tube"},"content":{"rendered":"\n<p><strong>Gagan GARG, Viren MENEZES, Upendra V BHANDARKAR, Bhalchandra P PURANIK, Rho Shin MYONG<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: N\/A<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2024-199<\/strong><\/p>\n\n\n\n<p>The ignition delay of various nano-fuels was compared with the base fuel (i.e. aircraft turbine engine fuel) to study the feasibility of use in high-speed aerospace applications (i.e. pulse detonation engines). The base fuel was mixed with two different nano-particles, titanium dioxide (TiO2) and multi-walled carbon nanotube (MWCNT), to develop a nano-fuel that can be employed for regenerative cooling of combustor walls before injection. A shock tube was employed to carry out the experiments where the liquid fuel was introduced in the test section as a wall droplet. From the experiments, an increase in the ignition delay was observed for the titanium dioxide nano-fuel whereas a slight reduction in the ignition delay was observed for the MWCNT nano-fuel.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/06\/HiSST-2024-199.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Gagan GARG, Viren MENEZES, Upendra V BHANDARKAR, Bhalchandra P PURANIK, Rho Shin MYONG<\/b><\/p>\n<p>DOI Number: N\/A<\/p>\n<p>Conference number: HiSST-2024-199<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1407,1414],"tags":[1719,1716,1718,1717],"class_list":["post-17056","post","type-post","status-publish","format-standard","hentry","category-events","category-11-hisst-2024","category-propulsion-systems-and-components-11-hisst-2024","tag-alternative-fuel","tag-ignition-delay","tag-nano-fuel","tag-pulse-detonation","category-993","category-1407","category-1414","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17056","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=17056"}],"version-history":[{"count":2,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17056\/revisions"}],"predecessor-version":[{"id":20808,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17056\/revisions\/20808"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=17056"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=17056"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=17056"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}