Purpose A combustor design is a particularly important and difficult task in the development
of gas turbine engines. During studies for accurate and easy combustor design, reasonable …

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 …

Abstract Full-scale Computational Fluid Dynamics (CFD) numerical simulations can
accurately predict the heat flux and metal wall temperature of gas turbine combustor liners …

This study deals with sliding-mode nonlinear observers for a flux-controlled active magnetic
bearing (AMB) operated with zero-bias flux. The Lyapunov sliding-mode observer (LSMO) …

A low-order model is proposed to predict the temperature of a multi-perforated plate from an
unresolved adiabatic computation. Its development relies on the analysis of both an …

Lean burn combustion is increasing its popularity in the aeronautical framework due to its
potential in reducing drastically pollutant emissions (NOx and soot in particular). Its …

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 …

Lean burn combustion is increasing its popularity in the aeronautical framework due to its
potential in reducing drastically pollutant emissions (NOx and soot in particular). Its …