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Review on research progress in liquid jet in crossflow
D Zhou, J Chang, C Tang, L He - International Communications in Heat and …, 2023 - Elsevier
Liquid jet in crossflow (LJIC) is an important subject of fluid mechanics, which is considered
as an effective method of fuel atomization in aircraft and widely used in gas turbine engine …
as an effective method of fuel atomization in aircraft and widely used in gas turbine engine …
Computational investigation of multi hydrogen jets at inclined supersonic flow
Scramjet design is directly associated with the fuel mixing inside the combustor. In this study,
the influences of the free stream angle on the fuel mixing zone of eight microjets are fully …
the influences of the free stream angle on the fuel mixing zone of eight microjets are fully …
Numerical simulation of the hydrogen mixing in downstream of lobe strut at supersonic flow
In this work, a computational fluid dynamic approach is employed to investigate the flow and
mixing characteristics of the fuel jet released from the trailing edge of the lobe strut at the …
mixing characteristics of the fuel jet released from the trailing edge of the lobe strut at the …
Effect of free stream angle on mixing performance of hydrogen multi-jets in supersonic combustion chamber
The fuel mixing process within the combustion chamber is a critical procedure for advance of
scramjet engine. In current study, the influence of free stream angle on the fuel mixing …
scramjet engine. In current study, the influence of free stream angle on the fuel mixing …
Effect of inclined block on fuel mixing of multi hydrogen jets in scramjet engine
Penetration and distribution of fuel inside the supersonic combustor significantly influence
on the overall performance of the scramjet. This research employed the numerical technique …
on the overall performance of the scramjet. This research employed the numerical technique …
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 …
are discussed. The effects of particle size and induced shock wave on flow and mixing …
Control mechanism of the three-dimensional shock wave/boundary layer interaction with the steady and pulsed micro-jets in a supersonic crossflow
Z Du, C Shen, W Huang, B Fan, Y Han - Physics of Fluids, 2022 - pubs.aip.org
The separation induced by shock wave/boundary layer interactions (SWBLI) is detrimental to
the performance of the flow field, and thus, needs to be reduced by using passive or active …
the performance of the flow field, and thus, needs to be reduced by using passive or active …
Influence of backward-facing step on the mixing efficiency of multi microjets at supersonic flow
The injection of the fuel is a highly important process for the enhancement of the scramjets.
In this article, the presence of the backward-facing step on the mixing of the multi-fuel jets is …
In this article, the presence of the backward-facing step on the mixing of the multi-fuel jets is …
Effect of fuel injection distance and cavity depth on the mixing and combustion characteristics of a scramjet combustor with a rear-wall-expansion cavity
The mixing and combustion characteristics of a model scramjet combustor with a rear-wall-
expansion cavity under a Mach 2.0 inflow are experimentally and numerically investigated …
expansion cavity under a Mach 2.0 inflow are experimentally and numerically investigated …
Investigation on the impact of the induced shock wave on the hydrogen mixing augmentation in a supersonic crossflow: A numerical study
Z Du, C Shen, W Huang, Y Han - Fuel, 2022 - Elsevier
The mixing process between the fuel and the incoming air flow plays an important role for
the engineering implementation of a scramjet engine. In the current study, the shock …
the engineering implementation of a scramjet engine. In the current study, the shock …