The rotating detonation engine is a promising realization of pressure gain combustion for propulsion and power generation systems. A rotating detonation engine running on ethylene-oxygen is simulated by using AMROC with a second-order accurate finite volume method and approximate Riemann solvers. Multi-step chemical kinetic mechanisms are employed with a splitting approach. The rotating detonation is studied in a 2-D unwrapped chamber with premixed and non-premixed injections and is then simulated in a 3-D annular chamber. The results show that using the adaptive mesh refinement method can simulate rotating detonation problems efficiently
Experimental and numerical study of rotating detonation is presented. The experimental study is focu...
A practical thermodynamic cycle model of a rotating detonation engine (RDE) is developed for the pur...
Rotating detonation engine is a new concept engine driven by detonation combustion for aerospace veh...
This paper describes the development of a computational code REFLOPS USG (REactive FLOw solver for P...
The aim of this work was to create an efficient tool for transient threedimensio...
A series of 3- and 2-dimensional numerical simulations of a rotating detonation engine (RDE) are car...
Based on summary and analysis of existing results and conclusions on rotating detonation wave in ann...
The potential higher performance of rotating detonation engines (RDEs), due to the constant volume c...
As turbine and rocket engine technology matures, performance increases between successive generation...
This article presents a three-dimensional (3D) numerical study on rotating detonation engine (RDE), ...
A two-dimensional, computational fluid dynamic (CFD) simulation of a semi-idealized rotating detonat...
This paper aims to adopt the method of injection via an array of holes in three-dimensional numerica...
A fast model of a Rotating Detonation Combustor (RDC) is developed based on the Method of Characteri...
From 2010 Warsaw University of Technology (WUT) and Institute of Aviation (IoA) jointly implement th...
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...
A practical thermodynamic cycle model of a rotating detonation engine (RDE) is developed for the pur...
Rotating detonation engine is a new concept engine driven by detonation combustion for aerospace veh...
This paper describes the development of a computational code REFLOPS USG (REactive FLOw solver for P...
The aim of this work was to create an efficient tool for transient threedimensio...
A series of 3- and 2-dimensional numerical simulations of a rotating detonation engine (RDE) are car...
Based on summary and analysis of existing results and conclusions on rotating detonation wave in ann...
The potential higher performance of rotating detonation engines (RDEs), due to the constant volume c...
As turbine and rocket engine technology matures, performance increases between successive generation...
This article presents a three-dimensional (3D) numerical study on rotating detonation engine (RDE), ...
A two-dimensional, computational fluid dynamic (CFD) simulation of a semi-idealized rotating detonat...
This paper aims to adopt the method of injection via an array of holes in three-dimensional numerica...
A fast model of a Rotating Detonation Combustor (RDC) is developed based on the Method of Characteri...
From 2010 Warsaw University of Technology (WUT) and Institute of Aviation (IoA) jointly implement th...
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...
A practical thermodynamic cycle model of a rotating detonation engine (RDE) is developed for the pur...
Rotating detonation engine is a new concept engine driven by detonation combustion for aerospace veh...