Experimental Investigation on the Wave Rotor Constant Volume Combustor

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dc.contributor.authorMatsutomi, Yu
dc.contributor.authorMeyer, Scott
dc.contributor.authorWijeyakulasuriya, Sameera
dc.contributor.authorIzzy, Zuhair
dc.contributor.authorNalim, M. Razi
dc.contributor.authorShimo, Masayoshi
dc.contributor.authorKowalkowski, Mike
dc.contributor.authorSnyder, Philip
dc.contributor.departmentMechanical Engineering, School of Engineering and Technologyen_US
dc.date.accessioned2019-06-14T21:33:56Z
dc.date.available2019-06-14T21:33:56Z
dc.date.issued2010-07-25
dc.description.abstractA wave rotor constant volume combustor was designed and built as a collaborative work of Rolls-Royce, Indiana University-Purdue University Indianapolis (IUPUI), and Purdue University. The experiment was designed to operate at rotational speeds of up to 4,200 rpm with air mass flow rates of approximately 18 lbm per second. Initial tests were conducted at 2,100 rpm with ethylene as fuel. The rig was operated with different fuel injection schemes to investigate operational characteristics of the combustor. Successful combustion and pressure gain were achieved over a range of operating conditions.en_US
dc.eprint.versionAuthor's manuscripten_US
dc.identifier.citationMatsutomi, Y., Meyer, S., Wijeyakulasuriya, S., Izzy, Z., Nalim, M., Shimo, M., … Snyder, P. (2010). Experimental Investigation on the Wave Rotor Constant Volume Combustor. In Joint Propulsion Conferences. 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. https://doi.org/10.2514/6.2010-7043en_US
dc.identifier.urihttps://hdl.handle.net/1805/19619
dc.language.isoen_USen_US
dc.publisherAIAAen_US
dc.relation.isversionof10.2514/6.2010-7043en_US
dc.relation.journal46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibiten_US
dc.sourceAuthoren_US
dc.subjectwave rotorsen_US
dc.subjectcombustionen_US
dc.subjectconstant volume combustoren_US
dc.titleExperimental Investigation on the Wave Rotor Constant Volume Combustoren_US
dc.typeArticleen_US
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