This paper aims to evaluate the accuracy and efficiency of different numerical simulation
approaches on cooling performance for the angled effusion cooling holes applied in a micro …

In this work, an in-house developed multiphysics unsteady approach (U-THERM3D) is
employed to compute wall temperatures in a loosely coupled manner for a model aero …

Conjugate heat transfer characteristics of the effusion cooling applied on the swirl-stabilized
combustor liner is experimentally and numerically investigated in a three-nozzle gas turbine …

The importance of the combustion chamber has been underestimated for years by
aeroengine manufacturers that focused their research efforts mainly on other components …

Computational fluid dynamics (CFD) plays a crucial role in the design of cooling systems in
gas turbine combustors due to the difficulties and costs related to experimental …

The accurate prediction of heat fluxes and, thus, metal wall temperatures of gas turbine (GT)
combustor liners is a complicated and numerically expensive task. Computational Fluid …

Computational fluid dynamics play a crucial role in the design of cooling systems in gas
turbine combustors due to the difficulties and costs related to experimental measurements …

Computational Fluid Dynamics is a fundamental tool to simulate the flow field and the multi-
physics nature of the phenomena involved in gas turbine combustors, supporting their …

1-D codes are still much utilized regarding the preliminary design and the design phase of a
single component. In particular, combustors is one of the most critical component in gas …

To reach ambitious emission goals, the use of sustainable aviation fuels (SAFs) is a short-
term option in current aero engines. The combustion of such fuels can, due to their low soot …