Cellular architectures are promising in a variety of engineering applications due to attractive
material properties. Additive manufacturing has reduced the difficulty in the fabrication of …

The thermal interplay between the combustor and the turbine exerts remarkable effects on
the performance of an aero-engine. The non-uniform distributions of the temperature and …

Unsteady component interaction represents a crucial topic in turbomachinery design and
analysis. Combustor/turbine interaction is one of the most widely studied topics both using …

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 …

The adoption of lean-burn technology in modern aero-engines influences the already critical
aerothermal conditions at turbine entry, where the absence of dilution holes preserves the …

The flow at the combustor turbine interface of power generation gas turbines with can
combustors is characterized by high and nonuniform turbulence levels, lengthscales, and …

In order to deepen the knowledge of the interaction between modern lean burn combustors
and high pressure turbines, a real scale annular three sector combustor simulator has been …

With the generalization of Lean Burn combustors, the flow field entering the turbine tends to
feature higher levels of swirl, turbulence, while different hot streak patterns often emerge if …

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 …

Nowadays, engines powering modern and large commercial or military aircraft essentially
rely on gas turbine technologies. Since the first prototypes built in the 40's, the efficiency and …