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 …

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 …

A high-pressure vane (HPV) equipped with a realistic film-cooling configuration has been
studied. The vane is characterized by the presence of multiple rows of fan-shaped holes …

Due to its robustness and simplicity, the simple actuator disk is still the most used and
popular method for performance analysis of horizontal axis wind turbines. However, the hub …

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 precise prediction of the aerothermal conditions at the outlet of modern combustors of
aero engines is of primary interest in the aerothermal design of high‐pressure turbines. The …

With the increase of computational power, more sophisticated computational methods can
be used, larger systems simulated, and complex phenomena predicted more reliably …

The accurate description and flow calibration at the exit of a gas turbine combustor is a key
point of turbine design. Indeed, the temperature field at the turbine inlet directly impacts both …

A high-pressure vane equipped with a realistic film-cooling configuration has been studied.
The vane is characterized by the presence of multiple rows of fan-shaped holes along …