Aeroengine performance is determined by temperature and pressure profiles along various
axial stations within an engine. Given limited sensor measurements, we require a …

The ability to accurately characterize the thermal efficiency of turbine stages with cooled
components is essential to advance turbine technologies. There are many methods for …

We present an immersive environment where Virtual Reality (VR) is used to visualize the
performance of a fleet of aircraft engines. Our virtual environment uses 3D geometric …

In this second part of our two-part paper, we provide a detailed, frequentist framework for
propagating uncertainties within our multivariate linear least squares model. This permits us …

The measurement of stagnation temperature is important for turbomachinery applications as
it is used in the calculation of component efficiency and engine specific fuel consumption …

To achieve higher thermal efficiency, gas turbines operate at increasingly higher turbine
inlet temperatures, leading to the need for advanced cooling methods such as film cooling …

Gas turbines are used in a broad range of aerospace and land-based applications from
power generation to aviation, and their usage is projected to continue to grow. It is therefore …

The flow in gas turbines exhibits a highly unsteady, complex and nonuniform manner, which
presents two main challenges. Firstly, it introduces instrumentation errors, contributing to …

This paper introduces the Bayesian mass average and details its computation. Owing to the
complexity of flow in an engine and the limited instrumentation and the precision of the …

Gas turbines are used in a broad range of aerospace and land-based applications from
power generation to aviation, and their usage is projected to continue to grow. As a result, it …