Rotating detonation engine is a new concept engine driven by detonation combustion for aerospace vehicles. In this paper, three-dimensional numerical simulation was used to investigate the combustion process and kinetic properties of reactive flow within the combustion chamber. To utilize fine grid in simulation, it requires a significant amount of CPU Time to depict this combustion. With the help of NVIDIA's CUDA, the computation was discretized and distributed to multiple graphics processing units, making the computation time reasonable and tolerable. The present study showed both the way to map our model into CUDA programming and the performance of acceleration, explicating the details of CUDA programming for different types of data...
Detonation, a combustion phenomenon is a supersonic combustion wave which plays critical role in the...
The particle path tracking method is proposed and used in two-dimensional (2D) and three-dimensional...
A two-dimensional, computational fluid dynamic (CFD) simulation of a semi-idealized rotating detonat...
AbstractContinuous Detonation Engine is a new concept of a supersonic combustion engine for aerospac...
Graphic processing units (GPUs) are powerful graphics engines featuring high levels of parallelism a...
This paper describes the development of a computational code REFLOPS USG (REactive FLOw solver for P...
From 2010 Warsaw University of Technology (WUT) and Institute of Aviation (IoA) jointly implement th...
The aim of this work was to create an efficient tool for transient threedimensio...
A three-dimensional numerical simulation of continuous rotating detonation engine (CRDE), which is p...
The rotating detonation engine is a promising realization of pressure gain combustion for propulsion...
Numerical solution of reaction–diffusion equations in three dimensions is one of the most challengin...
A series of 3- and 2-dimensional numerical simulations of a rotating detonation engine (RDE) are car...
A three-dimensional simulation is performed to study rotating detonation engines (RDEs) with a hollo...
Based on the two-dimensional numerical simulation of continuously rotating detonations in an annular...
采用一步化学反应模型,基于任意坐标系下Euler控制方程,对连续旋转爆轰发动机(CRDE)进行了三维数值模拟研究,详细分析了来流总压对CRDE参数特性的影响.研究发现:随着来流总压的增大,爆轰波峰值随...
Detonation, a combustion phenomenon is a supersonic combustion wave which plays critical role in the...
The particle path tracking method is proposed and used in two-dimensional (2D) and three-dimensional...
A two-dimensional, computational fluid dynamic (CFD) simulation of a semi-idealized rotating detonat...
AbstractContinuous Detonation Engine is a new concept of a supersonic combustion engine for aerospac...
Graphic processing units (GPUs) are powerful graphics engines featuring high levels of parallelism a...
This paper describes the development of a computational code REFLOPS USG (REactive FLOw solver for P...
From 2010 Warsaw University of Technology (WUT) and Institute of Aviation (IoA) jointly implement th...
The aim of this work was to create an efficient tool for transient threedimensio...
A three-dimensional numerical simulation of continuous rotating detonation engine (CRDE), which is p...
The rotating detonation engine is a promising realization of pressure gain combustion for propulsion...
Numerical solution of reaction–diffusion equations in three dimensions is one of the most challengin...
A series of 3- and 2-dimensional numerical simulations of a rotating detonation engine (RDE) are car...
A three-dimensional simulation is performed to study rotating detonation engines (RDEs) with a hollo...
Based on the two-dimensional numerical simulation of continuously rotating detonations in an annular...
采用一步化学反应模型,基于任意坐标系下Euler控制方程,对连续旋转爆轰发动机(CRDE)进行了三维数值模拟研究,详细分析了来流总压对CRDE参数特性的影响.研究发现:随着来流总压的增大,爆轰波峰值随...
Detonation, a combustion phenomenon is a supersonic combustion wave which plays critical role in the...
The particle path tracking method is proposed and used in two-dimensional (2D) and three-dimensional...
A two-dimensional, computational fluid dynamic (CFD) simulation of a semi-idealized rotating detonat...