Advances in plasma-assisted ignition and combustion for combustors of aerospace engines

M Li, Z Wang, R Xu, X Zhang, Z Chen… - Aerospace Science and …, 2021 - Elsevier
The improvement of the ignition and combustion performance of aerospace engines under
extreme conditions such as high altitude, low temperature, low pressure, and high speed is …

[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 …

Morphology of oblique detonation waves in a stoichiometric hydrogen–air mixture

H Teng, C Tian, Y Zhang, L Zhou… - Journal of Fluid …, 2021 - cambridge.org
Although the morphology of oblique detonation waves (ODWs) has been widely studied, it
remains impossible to predict the wave systems in the initiation region, which is a critical …

Experimental study on suppressing pressure feedback and combustion product backflow of the rotating detonation engine

X Yang, F Song, Y Wu, J Zhou, X Chen, J Kang… - Aerospace Science and …, 2023 - Elsevier
To further improve the feedback suppression effect of rotating detonation engines (RDEs),
an optimized Tesla valve inlet structure (TVI-II) was designed on the basis of the previous …

Numerical investigation on the combustion characteristics of aluminum powder fuel in a supersonic cavity-based combustor

Y Feng, S Luo, J Song, K Xia, D Xu - Applied Thermal Engineering, 2023 - Elsevier
In order to explore the propulsion performance and combustion organization rules of powder
fueled scramjets, research on powder fuel combustion characteristics in a supersonic cavity …

Numerical investigation on flow and mixing characteristics of powder fuel under strong shear and shock wave interaction

Y Feng, S Luo, J Song, D Xu - Energy, 2023 - Elsevier
In this investigation, the mixing process of powder fuel transverse jet and supersonic airflow
are discussed. The effects of particle size and induced shock wave on flow and mixing …

Intelligent reconstruction algorithm of hydrogen-fueled scramjet combustor flow based on knowledge distillation model compression

Y Tian, G Wang, X Deng, M Guo, H Ren, L Li… - International Journal of …, 2024 - Elsevier
The real-time perception of the combustion flow of a scramjet can help to quickly evaluate
the working state and provide a new opportunity for the intelligent reconstruction of the data …

Atomization of a liquid jet in supersonic crossflow in a combustion chamber with an expanded section

J Zhao, YJ Ren, Y Tong, W Lin, W Nie - Acta Astronautica, 2021 - Elsevier
The diffusion process and spatial distribution of a liquid jet in supersonic crossflow (Mach
number of 2) in a model combustor with an expanded section were investigated on the basis …

Multi-channel gliding arc plasma-assisted ignition in a kerosene-fueled model scramjet engine

R Feng, Z Wang, M Sun, H Wang, Y Huang… - Aerospace Science and …, 2022 - Elsevier
A multi-channel gliding arc (MCGA) plasma was utilized to ignite a kerosene-fueled model
scramjet engine with an inflow of Ma2. 92. High-speed photography from the top and side …

Progress and prospects of artificial intelligence development and applications in supersonic flow and combustion

J Le, M Yang, M Guo, Y Tian, H Zhang - Progress in Aerospace Sciences, 2024 - Elsevier
Due to the significant improvement in computing power and the rapid advancement of data
processing technologies, artificial intelligence (AI) has introduced new tools and …