Convection of a hot spot through the interface between the combustion chamber and the turbine
Convection of a hot spot through the interface between the combustion chamber and the turbine
As part of the EmBreCOfF project (Low-emission combustion chamber system for CO2-free flight), the Institute of Propulsion Technology is conducting research into advanced technologies for flexible fuels.
Credit: DLR (CC BY-NC-ND 3.0)