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 …

Recent advances in cavity-based scramjet engine-a brief review

G Choubey, Y Devarajan, W Huang, K Mehar… - International Journal of …, 2019 - Elsevier
At present, the critical issue related to design of scramjet engine is to achieve efficient mixing
between the air and fuel. Among the several fuel injection strategies, cavity flame holder is …

Research progress on strut-equipped supersonic combustors for scramjet application

J Chang, J Zhang, W Bao, D Yu - Progress in Aerospace Sciences, 2018 - Elsevier
Scramjets are regarded as one of the most efficient air-breathing propulsion devices in
supersonic flight conditions, and combustors are critical components in scramjet engines …

Numerical investigation on geometric sensitivity and flame stabilisation mechanism in H2 fueled two-strut based scramjet combustor

G Choubey, P Gaud, AM Fatah, Y Devarajan - Fuel, 2022 - Elsevier
The layout of the strut fuel injector has a significant impact on the flame stabilization process
of the strut-based scramjet combustor. That's why a two-strut-based scramjet model has …

A review of aircraft subsonic and supersonic combustors

GAQ Abdulrahman, NAA Qasem, B Imteyaz… - Aerospace Science and …, 2023 - Elsevier
Combustion is an essential process for generating propulsion for most existing aircraft. The
combustion processes, such as ignition, flame propagation, and flame stability, are …

Flame stabilization and local combustion modes in a cavity-based scramjet using different fuel injection schemes

D Cao, HE Brod, N Yokev, D Michaels - Combustion and Flame, 2021 - Elsevier
This paper investigates the impact of fuel distribution on flame stabilization and local
combustion modes in a cavity-based scramjet. Two injection schemes with a global …

Direct numerical simulation of supersonic internal flow in a model scramjet combustor under a non-reactive condition

J Fang, X Deng, ZX Chen - Physics of Fluids, 2023 - pubs.aip.org
A Mach 1.5 non-reactive flow in a cavity-stabilized combustor of a model scramjet is studied
via a direct-numerical simulation approach, and the analysis is focused on the interaction …

Survey on the mode transition technique in combined cycle propulsion systems

W Huang, L Yan, J Tan - Aerospace Science and Technology, 2014 - Elsevier
With the maturation of the scramjet technologies, the urgent development of the combined
cycle propulsion system has been put forward, and it can help the vehicle to launch and land …

Advances and challenges in modeling high-speed turbulent combustion in propulsion systems

ED Gonzalez-Juez, AR Kerstein, R Ranjan… - Progress in Energy and …, 2017 - Elsevier
Combustion environments in propulsion systems involve the interaction of a variety of
physics. In devices such as augmentors, ramjets and scramjets, such environments include …

[HTML][HTML] Review of atomization mechanism and spray characteristics of a liquid jet in supersonic crossflow

Z Yaozhi, CAI Zun, LI Qinglian, LI Chenyang… - Chinese Journal of …, 2023 - Elsevier
The injection and atomization process of a liquid fuel jet is critical for an ignition start of a
scramjet engine. Airwall-mounted crossflow injection strategy is widely used in scramjet …