INSPIRE

INSpiring Pressure gain combustion Integration, Research, and Education

Marie Curie Innovative Training Network (ITN)

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RoDavGT

Rotierende Detonationsverbrennung in Gasturbinen-Flugtriebwerken

Luftfahrtforschungsprogramm V-3

One of the main challenges in the practical implementation of Pressure Gain Combustion (PGC) into gas turbines is the lack of designs for turbomachines that can cope efficiently with the PGC exhaust gas. Although still a topic of active research, it is generally accepted that conventional turbine expanders interacting with the exhaust of pressure gain combustors will have lower isentropic efficiency, compared to their design operation. In this project, we are investigating unsteady flow field exhausting from PGC and trying to develop a turbine design methodology specifically for this harsh inflow. 

Kontakt: Eric Bach

Einstein Foundation Berlin

Visiting Fellowship - Effie Gutmark

Einstein Foundation Berlin

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