Recently developed lean-burn combustors offer reduced NO x emissions for gas turbines.
The flow at exit of lean-burn combustors is dominated by hot streaks and residual swirl …

In mass customization, a manufacturing line is required to be kept in reliable operation to
handle product demand volatility and potential machine degradations. Recent advances in …

Advanced civil aero-engines tend to adopt lean burn combustors to meet emission
requirements. The exit of a lean burn combustor experiences highly non-uniformities in both …

The computational and experimental assessment of a lean-burn low-NOx combustor
simulator for an engine component test facility is presented. The Engine Component Aero …

The combustor-turbine interface in a gas turbine is characterised by complex, highly
unsteady flows. In a combined experimental and large eddy simulation (LES) study …

Combustion–turbine interaction phenomena are attracting ever-growing interest in recent
years. As a matter of fact, the strong unsteady and three-dimensional flow field that …

The complex flow field of gas turbine lean combustors is meant to reduce NOx emissions
and maintain a stable flame by controlling the local temperature and promoting high …

The pronounced nonuniform temperature distribution in the core engine flow path is a
recurring problem of gas turbine engine design process. Specifically, turbine entry …

Following the industrial trend of increasingly integrative design and analysis of the
combustor-turbine interface, the EC FP7 project FACTOR was launched many years ago …

Lean-premixed combustion technologies have been widely adopted in advanced civil
turbofan engine to reduce NOx emission. There exist hot streak (HS) and swirl …