Review of combustion stabilization for hypersonic airbreathing propulsion

Q Liu, D Baccarella, T Lee - Progress in Aerospace Sciences, 2020 - Elsevier
A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …

Plasma assisted combustion: Dynamics and chemistry

Y Ju, W Sun - Progress in Energy and Combustion Science, 2015 - Elsevier
Plasma assisted combustion is a promising technology to improve engine performance,
increase lean burn flame stability, reduce emissions, and enhance low temperature fuel …

Plasma-assisted ignition and combustion

A Starikovskiy, N Aleksandrov - Progress in Energy and Combustion …, 2013 - Elsevier
The use of a thermal equilibrium plasma for combustion control dates back more than a
hundred years to the advent of internal combustion (IC) engines and spark ignition systems …

Plasma-assisted ignition and combustion: nanosecond discharges and development of kinetic mechanisms

SM Starikovskaia - Journal of Physics D: Applied Physics, 2014 - iopscience.iop.org
This review covers the results obtained in the period 2006–2014 in the field of plasma-
assisted combustion, and in particular the results on ignition and combustion triggered or …

A review of recent studies and emerging trends in plasma-assisted combustion of ammonia as an effective hydrogen carrier

ZA Shah, G Mehdi, PM Congedo, D Mazzeo… - International Journal of …, 2024 - Elsevier
Recently, ammonia is getting more attractive as a potential alternative fuel for future power
generation and transportation purposes due to its ability to reduce consumption of fossil …

Ignition and combustion enhancement in a cavity-based supersonic combustor by a multi-channel gliding arc plasma

R Feng, Y Huang, J Zhu, Z Wang, M Sun… - … Thermal and Fluid …, 2021 - Elsevier
A multi-channel gliding arc (MCGA) plasma was used to enhance ignition and combustion of
ethylene fuel in a cavity-based scramjet combustor with an inflow speed of Ma= 2.92 …

Combustion enhancement in a model scramjet by a simple pin-to-pin AC arc plasma

Y Tian, J Zhu, M Sun, M Wan, Y Sun, B Yan… - Proceedings of the …, 2024 - Elsevier
A simple pin-to-pin alternative-current (AC) arc plasma located upstream of the cavity was
developed to achieve significant combustion enhancement in a Mach 2.52 C 2 H 4-fueled …

Suppression of combustion mode transitions in a hydrogen-fueled scramjet combustor by a multi-channel gliding arc plasma

R Feng, J Zhu, Z Wang, F Zhang, Y Ban, G Zhao… - Combustion and …, 2022 - Elsevier
A multi-channel gliding arc (MCGA) plasma was utilized to suppress combustion mode
transition in a hydrogen-fueled cavity-based scramjet combustor with an inflow speed of …

Unstart phenomena induced by flow choking in scramjet inlet-isolators

S Im, H Do - Progress in Aerospace Sciences, 2018 - Elsevier
A review of recent research outcomes in downstream flow choking-driven unstart is
presented. Unstart is a flow phenomenon at the inlet that severely reduces the air mass flow …

An exploration of inter-pulse coupling in nanosecond pulsed high frequency discharge ignition

JK Lefkowitz, T Ombrello - Combustion and Flame, 2017 - Elsevier
A parametric exploration of the dynamics of ignition using nanosecond pulsed high
frequency discharges (NPHFD) in flowing mixtures of methane and air is conducted to …