This paper aims to adopt the method of injection via an array of holes in three-dimensional numerical simulations of a rotating detonation engine (RDE). The calculation is based on the Euler equations coupled with a one-step Arrhenius chemistry model. A pre-mixed stoichiometric hydrogen-air mixture is used. The present study uses a more practical fuel injection method in RDE simulations, injection via an array of holes, which is different from the previous conventional simulations where a relatively simple full injection method is usually adopted. The computational results capture some important experimental observations and a transient period after initiation. These phenomena are usually absent in conventional RDE simulations due to the us...
High-fidelity numerical simulations of an experimental rotating detonation engine with discrete fuel...
As the injection total pressure increases, the flow field in the combustion chamber of rotating deto...
Two-dimensional rotating detonation waves (RDWs) with separate injections of hydrogen and air are si...
This article presents a three-dimensional (3D) numerical study on rotating detonation engine (RDE), ...
Previous numerical simulations of the hydrogen-air rotating detonation engine have been carried out ...
The potential for a continuous detonation wave in rotating detonation engine (RDE) hugely rely on th...
Three-dimensional numerical simulation of a rotating detonation engine (RDE) is carried out in coaxi...
Three-dimensional numerical simulation of a rotating detonation engine (RDE) is carried out in coaxi...
Experimental and numerical study of rotating detonation is presented. The experimental study is focu...
From 2010 Warsaw University of Technology (WUT) and Institute of Aviation (IoA) jointly implement th...
In light of the growing demand for more efficient aviation engines, detonation-based engines are bei...
A series of 3- and 2-dimensional numerical simulations of a rotating detonation engine (RDE) are car...
Two-dimensional numerical simulations are performed to investigate the effects of spatially discrete...
The potential higher performance of rotating detonation engines (RDEs), due to the constant volume c...
The efficiency of a Rotating Detonation Combustor (RDC) strongly depends on the transitory injection...
High-fidelity numerical simulations of an experimental rotating detonation engine with discrete fuel...
As the injection total pressure increases, the flow field in the combustion chamber of rotating deto...
Two-dimensional rotating detonation waves (RDWs) with separate injections of hydrogen and air are si...
This article presents a three-dimensional (3D) numerical study on rotating detonation engine (RDE), ...
Previous numerical simulations of the hydrogen-air rotating detonation engine have been carried out ...
The potential for a continuous detonation wave in rotating detonation engine (RDE) hugely rely on th...
Three-dimensional numerical simulation of a rotating detonation engine (RDE) is carried out in coaxi...
Three-dimensional numerical simulation of a rotating detonation engine (RDE) is carried out in coaxi...
Experimental and numerical study of rotating detonation is presented. The experimental study is focu...
From 2010 Warsaw University of Technology (WUT) and Institute of Aviation (IoA) jointly implement th...
In light of the growing demand for more efficient aviation engines, detonation-based engines are bei...
A series of 3- and 2-dimensional numerical simulations of a rotating detonation engine (RDE) are car...
Two-dimensional numerical simulations are performed to investigate the effects of spatially discrete...
The potential higher performance of rotating detonation engines (RDEs), due to the constant volume c...
The efficiency of a Rotating Detonation Combustor (RDC) strongly depends on the transitory injection...
High-fidelity numerical simulations of an experimental rotating detonation engine with discrete fuel...
As the injection total pressure increases, the flow field in the combustion chamber of rotating deto...
Two-dimensional rotating detonation waves (RDWs) with separate injections of hydrogen and air are si...