Effects of different hole structures of pre-chamber with turbulent jet ignition on the flame propagation and lean combustion performance of a single-cylinder engine

L Zhou, Y Song, J Hua, F Liu, Z Liu, H Wei - Fuel, 2022 - Elsevier
Turbulent jet ignition is an advanced pre-chamber approach for improving combustion rates
and extending lean burn limitations. The hot flows jetted from the pre-chamber through jet …

The ignition characteristics of the pre-chamber turbulent jet ignition of the hydrogen and methane based on different orifices

P Liu, L Zhong, L Zhou, H Wei - International Journal of Hydrogen Energy, 2021 - Elsevier
In this paper, the combustion characteristics of premixed CH 4-air and H 2-air mixtures with
different excess air coefficients ignited by hot jet or jet flame are investigated experimentally …

Prechamber ignition: An exploratory 2-D DNS study of the effects of initial temperature and main chamber composition

S Benekos, CE Frouzakis, GK Giannakopoulos… - Combustion and …, 2020 - Elsevier
A numerical investigation was conducted to study ignition and the initial phases of methane
combustion in a two-dimensional setup consisting of a pre-(PC) and main (MC) chamber …

Direct numerical simulations and models for hot burnt gases jet ignition

Q Malé, O Vermorel, F Ravet, T Poinsot - Combustion and Flame, 2021 - Elsevier
This work uses multiple three-dimensional Direct Numerical Simulations (DNSs) to i)
investigate the ignition process of a cold lean premixed mixture at atmospheric conditions by …

A data-driven approach using machine learning for early detection of the lean blowout

VR Hasti, A Navarkar, JP Gore - Energy and AI, 2021 - Elsevier
A data-driven approach using machine learning is presented for the identification of the
critical flame location for the early detection of an incipient lean blowout (LBO) in a realistic …

[HTML][HTML] A 2-D DNS study of the effects of nozzle geometry, ignition kernel placement and initial turbulence on prechamber ignition

S Benekos, CE Frouzakis, GK Giannakopoulos… - Combustion and …, 2021 - Elsevier
A parametric direct numerical simulation study was conducted to investigate the effects of
the initial flow field (quiescent or turbulent), nozzle inlet sharpness and width, main chamber …

High-fidelity numerical simulation of longitudinal thermoacoustic instability in a high-pressure subscale rocket combustor

VR Hasti, R Ranjan - Aerospace Science and Technology, 2024 - Elsevier
A detailed analysis of thermoacoustic combustion instability in a subscale rocket combustor
at high pressure is reported in this paper using the high-fidelity large-eddy simulation (LES) …

Computation of conventional and alternative jet fuel sensitivity to lean blowout

VR Hasti, P Kundu, S Som, SH Won, FL Dryer… - Journal of the Energy …, 2022 - Elsevier
Abstract Large Eddy Simulations (LES) are performed to compute the sensitivity of a
conventional (A-2) and an alternate bio-jet (C-1) fuel to Lean Blowout (LBO). A realistic …

Numerical simulations and analysis of the turbulent flow field in a practical gas turbine engine combustor

VR Hasti, P Kundu, S Som… - Proceedings of the …, 2022 - journals.sagepub.com
The turbulent flow field in a practical gas turbine combustor is very complex because of the
interactions between various flows resulting from components like multiple types of swirlers …

Fundamental insights on turbulence characterization, vortex motion and ignition mechanism of sub/supersonic turbulent jet flames

G Li, H Sun, Q Tang, H Zhen, H Wang, H Liu… - Applied Thermal …, 2024 - Elsevier
This paper presents turbulence characterization and vortex behavior measurements of
sub/supersonic jet flames subjected to extreme levels of turbulence. Specifically …