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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 study on the transverse jet flow and mixing characteristics of hydrogen/metal powder fuel in powder fuel scramjet
H Ding, C Zhuo, X Chen, H Deng, M Li, B Sun, C Li - Fuel, 2022 - Elsevier
The powder fuel scramjet is one of the most promising propulsion systems for future
hypersonic vehicles. To study the flow mechanism and mixing characteristics of gas-particle …
hypersonic vehicles. To study the flow mechanism and mixing characteristics of gas-particle …
Numerical simulations of high frequency transverse pulsed jet injection into a supersonic crossflow
The design of scramjet engines includes the investigation of minimally intrusive fuel delivery
mechanisms which maximize jet fuel penetration and mixing. In subsonic crossflows it has …
mechanisms which maximize jet fuel penetration and mixing. In subsonic crossflows it has …
Effect of non-uniform incoming flow on the mixing enhancement in a scramjet cavity combustor
D Jian, Y Yude - International Journal of Hydrogen Energy, 2024 - Elsevier
Mixing in the combustion chamber is influenced by the velocity distribution of the inlet
airflow. Numerical simulations are carried out by using the 3D coupled implicit Reynolds …
airflow. Numerical simulations are carried out by using the 3D coupled implicit Reynolds …
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 …
[HTML][HTML] Effect of injection scheme on asymmetric phenomenon in rectangular and circular scramjets
MA Guangwei, SUN Mingbo, Z Guoyan, C Liang… - Chinese Journal of …, 2023 - Elsevier
The asymmetric separation has a crucial effect on the performance of the scramjet. In this
study, the asymmetric separation and combustion in both rectangular and circular scramjets …
study, the asymmetric separation and combustion in both rectangular and circular scramjets …
Experimental investigation of sonic transverse jets in Mach 5 crossflow
An experimental investigation of sonic transverse jets in Mach 5 cross flow over a flat plate
with a sharp leading edge was carried out. Jet to free stream momentum flux ratio, J, was …
with a sharp leading edge was carried out. Jet to free stream momentum flux ratio, J, was …
Large eddy simulation of non-reacting flow and mixing fields in a rotating detonation engine
Abstract Large Eddy Simulations (LES) of the non-reacting flow and mixing fields in a
Rotating Detonation Engine (RDE) from Air Force Research Laboratory (AFRL) are …
Rotating Detonation Engine (RDE) from Air Force Research Laboratory (AFRL) are …
Influence of the secondary flow control on the transverse gaseous injection flow field properties in a supersonic flow
The supersonic mixing process is a critical issue for the design of the scramjet engine. In this
paper, the secondary flow control concept has been proposed and studied in order to …
paper, the secondary flow control concept has been proposed and studied in order to …
Distribution characteristics and mixing mechanism of a liquid jet injected into a cavity-based supersonic combustor
Mechanism of the mixing process and distribution characteristics of a liquid jet injected into a
supersonic crossflow with a Mach number of 2.85 in a cavity-based combustor are …
supersonic crossflow with a Mach number of 2.85 in a cavity-based combustor are …