Investigation of flame flashback phenomenon in a supersonic crossflow with ethylene injection upstream of cavity flameholder

G Zhao, M Sun, J Wu, X Cui, H Wang - Aerospace Science and Technology, 2019 - Elsevier
In the present study, a flame flashback phenomenon inside an ethylene-fuelled scramjet
combustor equipped with a cavity flameholder is investigated under flight Mach 5.5 …

Effects of injection on flame flashback in supersonic crossflow

G Zhao, J Du, H Yang, T Tang, M Sun - Aerospace Science and …, 2022 - Elsevier
An approach that combines numerical, experimental, and theoretical analyses has been
implemented to investigate the effects of the injection parameters on the flame flashback …

Numerical study of periodic flame flashback in a cavity-based scramjet combustor

S Guo, X Zhang, Q Liu, L Yue - Physics of Fluids, 2023 - pubs.aip.org
The periodic flame flashback phenomenon in an ethylene-fueled cavity-based scramjet
combustor was numerically investigated by a three-dimensional unsteady Reynolds …

Numerical investigation of the scale effects of the flame flashback phenomenon in scramjet combustors

G Zhao, J Du, M Liu, H Wang, M Sun - Aerospace Science and Technology, 2021 - Elsevier
The scale effect of flame flashbacks inside an ethylene-fueled scramjet combustor was
investigated through an approach that combines numerical, experimental, and theoretical …

Experimental investigations of combustion oscillation modes in a large-aspect-ratio dual-mode combustor equipped with multi-strut

H Qiu, G Luan, G Feng, J Zhang, W Bao - Physics of Fluids, 2023 - pubs.aip.org
The annular scramjet combustor is considered one of the best configurations for a wide-
speed-range combined engine, owing to its superior thermal protection performance and …

Role of cavity in a Mach 8 axisymmetric scramjet combustor: Flame stabilization vs combustion enhancement

G Ma, G Zhao, M Sun, T Tang, F Li, D Xiong - Physics of Fluids, 2024 - pubs.aip.org
The cavity-assisted scramjet has been proven to be the most promising propulsion system
for air-breathing hypersonic vehicles. In this paper, numerical simulations of a Mach 8 …

Numerical investigation of combustion characteristics of upstream crescent cavities in a scramjet combustor

T Roos, A Pudsey, H Ogawa - Acta Astronautica, 2021 - Elsevier
This study investigates the combustion performance of a number of novel, crescent shaped
cavities placed directly in front of the fuel injection point in a scramjet combustor. Cavities …

Experimental investigations of cavity parameters leading to combustion oscillation in a supersonic crossflow

GY Zhao, MB Sun, XL Song, XP Li, HB Wang - Acta Astronautica, 2019 - Elsevier
The effects of cavity parameters on combustion oscillation inside an ethylene-fueled
scramjet combustor equipped with a cavity flameholder are experimentally investigated for …

Effect of boundary layer thickness on supersonic combustion in a scramjet combustor

F Li, G Zhao, Y Huang, D Yang, G Ma, Y Li… - Aerospace Science and …, 2023 - Elsevier
In this study, the effect of boundary layer thickness on supersonic combustion in an ethylene-
fueled scramjet combustor under Mach 5.5 flight conditions is studied by employing …

Investigation of oscillation modes in a high-speed flow with heat supply. I. Experiment

NN Fedorova, MA Goldfeld, VV Pickalov - Combustion, Explosion, and …, 2022 - Springer
Results of experimental investigations of the flow in a channel with sudden expansion
without and with heat supply into a supersonic air flow are presented. Based on processing …