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 …

Numerical simulation of multiple components in turbomachinery applications is very CPU-
demanding but remains necessary in the majority of cases to capture the proper coupling …

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 characterization of pressure, temperature and velocity fields in turbomachinery flows
typically relies on well-proven probe-based technology such as pneumatic probes, hot-wire …

The coupling between different components of a turbomachinery is becoming more widely
studied especially by use of computational fluid dynamics. Such simulations are of particular …

Within the scope of European Commission FP7 project FACTOR, dedicated to combustor-
turbine-interaction research, a clean-sheet design of a rotating turbine test rig featuring a …

Abstract Nozzle Guide Vanes aero-thermal performance is commonly assessed in the
industry using tangentially-averaged quantities, imposed at the combustor-turbine interface …

Reducing the uncertainties in the prediction of turbine inlet conditions is a crucial aspect to
improve aero engine designs and further increase engine efficiencies. To meet constantly …

Accurate prediction of thermal field in high pressure turbines is a critical aspect of
aerodynamic and durability design. This is particularly true when the flow at turbine inlet …

Erosion of compressor and turbine blades operating in extreme environment fouled with
sand particles, ash or soot is a serious problem for gas turbine manufacturers and users …