Hydrogen fuel in scramjet engines-a brief review

G Choubey, D Yuvarajan, W Huang, L Yan… - International Journal of …, 2020 - Elsevier
Due to the wide flammability range and low ignition delay of Hydrogen, it can burn rapidly
and generate a large amount of thrust. It is for this reason alone that many researchers have …

Recent research progress on transverse injection technique for scramjet applications-a brief review

G Choubey, D Yuvarajan, W Huang, A Shafee… - International Journal of …, 2020 - Elsevier
With the advancement of the air-breathing propulsion system, the supersonic vehicle
technique has drawn a significant interest worldwide. The mixing and combustion process in …

Numerical investigation on mixing improvement mechanism of transverse injection based scramjet combustor

G Choubey, PM Yadav, Y Devarajan, W Huang - Acta Astronautica, 2021 - Elsevier
The major hurdle in augmenting the performance of supersonic engines is the appropriate
distribution of injected fuel within the supersonic chamber. That's why SST k− ω model is …

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 …

Supersonic mixing in airbreathing propulsion systems for hypersonic flights

W Huang, Z Du, L Yan, Z Xia - Progress in Aerospace Sciences, 2019 - Elsevier
Achieving efficient fuel-air mixing is a crucial problem for the design of scramjet engines.
Due to the very short residence time of the fuel within the scramjet combustor for typical flight …

Effect of different strut design on the mixing performance of H2 fueled two-strut based scramjet combustor

G Choubey, M Solanki, O Patel, Y Devarajan, W Huang - Fuel, 2023 - Elsevier
Strut fuel injection approach significantly influences the combustion mechanism inside the
scramjet engines. To address this issue, researchers are nowadays mainly focused on a …

Effect of cavity back height on mixing efficiency of hydrogen multi-jets at supersonic combustion chamber

Y Jiang, A Poozesh, SM Marashi, R Moradi… - International Journal of …, 2020 - Elsevier
Stable fuel distribution and mixing is noteworthy for increasing the efficiency of the scramjet
engine at high-speed flight. In this work, numerical studies are accomplished to inspect and …

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 …

Computational investigation of multi-cavity fuel injection on hydrogen mixing at supersonic combustion chamber

Z Li, TD Manh, MB Gerdroodbary, ND Nam… - International Journal of …, 2020 - Elsevier
Enhancement of the mixing inside the combustor is a significant process for increasing the
efficiency of the scramjet. This work applied the computational method for the investigation …