Fiscal Year	2019
Division	Graduate School of Engineering & Applied Science
Department	Mechanical & Aerospace Engineering
Investigator(s)	Brophy, Christopher M.
Sponsor	Combustion Research and Flow Technology, Inc. (Other)
Summary	Main objective of this collaborative research is the development of design support tools and testing of Rotating Detonation Engines (RDEs) under rocket operating conditions. For RDEs to gain widespread adoption in rocket engine systems, they have to operate reliably over longer duration and over a wide range of conditions. This involves design of the injector systems, feed manifolds, sizing of the ROE, cooling mechanisms and design of the nozzle system.
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Publications	Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal
Data	Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal