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 …

Optical and numerical study on the effect of wall impingement on passive jet ignition characteristics of methane/air mixture

Y Zhang, X Ma, J Mao, Y Fang, C Jiang, Z Wang… - Fuel, 2024 - Elsevier
Pre-chamber turbulent jet ignition is a promising high-efficiency combustion technique to
achieve stable lean-burn operation for spark-ignition engines. Wall impingement by a high …

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 …

[HTML][HTML] A spark energy deposition model in mixture fraction space for simulations of turbulent non-premixed flame ignition

HSAM Awad, S Gkantonas, E Mastorakos - Applications in Energy and …, 2024 - Elsevier
Predicting the ignition probability remains important for designing reliable combustors. A
spark ignition model in mixture fraction space is proposed and used in a Large Eddy …

Analysis of mode transition in a rotating detonation engine combustor

VR Hasti, NO Attal, G Kumar - AIAA SCITECH 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1111. vid Numerical simulations
are performed for hydrogen-fueled rotating detonation engine combustor under two different …

Dynamically Dominant Flow Features During Wave Mode Transition in a Rotating Detonation Engine Combustor

VR Hasti, J Pratt, R Ranjan - AIAA SCITECH 2025 Forum, 2025 - arc.aiaa.org
In this study, we examine the spatio-temporal characteristics of dynamically dominant flow
features within a hydrogen-fueled rotating detonation engine (RDE) combustor. We utilized …

Computational study of longitudinal combustion instability in a high-pressure combustor

VR Hasti, R Ranjan - AIAA SCITECH 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-2087. vid In this study, results from
large-eddy simulation (LES) of self-sustained longitudinal combustion instability observed …

A reactor model of ignition in the head vortex of a hot puff injected into combustible mixture

ME Feyz, B Sule, MR Nalim - AIP Conference Proceedings, 2023 - pubs.aip.org
A suddenly starting transient turbulent jet or 'puff'of hot gas can ignite surrounding
combustible mixtures, such as in a closed-volume combustion engine. The puff can be …