Gas turbine combustor design is a complex multi-objective problem. In the present study,
parametric design space study and optimization of a gas turbine combustor using …

The majority of premixed industrial gas turbine combustion systems feature two or more
separately controlled fuel lines. Every additional fuel line improves the operational flexibility …

Model-based design optimization is a ubiquitous and powerful tool in many engineering
disciplines. Its application to industrial combustion has been quite limited, however, due in …

This work presents a data-driven optimization technique for the optimization of the flame
response within a low-order acoustic network model. The methodology exploits the Nyquist …

Current emission prediction models in the conceptual design phase are based on historical
data and empirical correlations. Two main reasons contributing to the current state of …

In this article, geometry optimization of a jet stirred reactor (JSR) combustor has been carried
out for minimum NO emissions in methane oxidation using a combined numerical algorithm …

The design of gas turbine combustors for optimal operation at different power ratings is a
multifaceted engineering task, as it requires the consideration of several objectives that must …

The aim of the project is to design an ultra-low emissions gas turbine combustor, comparing
to the current one that are installed in the aerospace industry. The type of combustor that …

In combustor design and development, the use of unsteady computational fluid dynamics
(CFD) simulations of transient combustor aero-thermo-dynamics to provide an insight into …

The preliminary design of gas turbine combustors is a multi-objective optimization problem.
The methodology to be used at the preliminary design stage depends on the freedom of …