Design methodology for combustor in advanced gas turbine engines: a review

I Kim, H Jin, K Ri, S Hyon, C Huang - Aircraft Engineering and …, 2024 - emerald.com
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 …

Influence of operating conditions on flow field dynamics and soot formation in an aero-engine model combustor

M Grader, P Gerlinger - Combustion and Flame, 2023 - Elsevier
Large-eddy simulations of a sooting aero-engine model combustor are performed for three
operating points. They are analyzed to investigate the influence of secondary air injection …

Comparison of adiabatic and conjugate heat transfer models on near-wall region flows and thermal characteristics of angled effusion cooling holes

C Zong, C Ji, J Cheng, T Zhu - Thermal Science and Engineering Progress, 2022 - Elsevier
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 …

Assessment of radiative heat transfer with/without turbulence-radiation interaction in aero-engine swirling combustors of different geometric scales

G Liu, J Zhu, Y Liu - Applied Thermal Engineering, 2024 - Elsevier
Radiative heat transfer (RHT) and Turbulence-Radiation Interaction (TRI) are closed related
with the internal temperature, NO formation and liner temperature of aero-engine …

Spectral effects of radiating gases and soot on an experimental aero-engine combustion chamber using full-spectrum k-distribution method

C Wang, H Di, H Lin, S Shang, L Yang - Applied Thermal Engineering, 2024 - Elsevier
Radiative heat transfer is the main mode of heat transfer and has been proven to be
important in the aero-engine combustion. Those radiating gases and soot resulted from …

The Italian research on HPC key technologies across EuroHPC

M Aldinucci, G Agosta, A Andreini… - Proceedings of the 18th …, 2021 - dl.acm.org
High-Performance Computing (HPC) is one of the strategic priorities for research and
innovation worldwide due to its relevance for industrial and scientific applications. We …

Assessment of a conjugate heat transfer method on an effusion cooled combustor operated with a swirl stabilized partially premixed flame

A Amerini, S Paccati, L Mazzei… - Journal of …, 2023 - asmedigitalcollection.asme.org
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 …

Computational Optimization of a Loosely-Coupled Strategy for Scale-Resolving CHT CFD Simulation of Gas Turbine Combustors

A Amerini, S Paccati, A Andreini - Energies, 2023 - mdpi.com
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 …

Assessment of a conjugate heat transfer method on an effusion cooled combustor operated with a swirl stabilized partially premixed flame

A Amerini, S Paccati, L Mazzei… - … Expo: Power for …, 2022 - asmedigitalcollection.asme.org
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 …

Prediction of liner metal temperature of an aeroengine combustor with multi-physics scale-resolving CFD

D Bertini, L Mazzei, A Andreini - Entropy, 2021 - mdpi.com
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 …