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 …

High-pressure turbine (HPT) rotor blades work in a harsh environment with high temperature
and rotational speed. Affected by blade row interaction and inlet non-uniformities, the rotor …

The higher demand for temperature rises and low-pollution combustion methods make it
more problematic to regulate the outlet temperature distribution (OTD) of advanced gas …

When the high-pressure turbine guide blade works in the aero-engine, it is in the complex
gas-heat environment of the combustion chamber and the turbine. The temperature …

In new generation aero-engines, lean-burn combustors are equipped with swirl injectors in
order to reduce pollutant emissions. At the exit of these combustors, the flow is dominated by …

A laboratory-scale gas turbine model combustor fueled with methane is studied
experimentally with the aid of three-dimensional computed tomography of …

Rapidly predicting the temperature field of the aero-engine combustion chamber can assist
researchers in quickly understanding the combustion state. Although deep learning methods …

Using the inlet flow parameters to get the temperature field of the aero-engine combustor
can help researchers quickly learn about the combustion state of the combustor, which is …

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 …