A two-dimensional, computational fluid dynamic (CFD) simulation of a semi-idealized rotating detonation engine (RDE) is described. The simulation operates in the detonation frame of reference and utilizes a relatively coarse grid such that only the essential primary flow field structure is captured. This construction yields rapidly converging, steady solutions. Results from the simulation are compared to those from a more complex and refined code, and found to be in reasonable agreement. The performance impacts of several RDE design parameters are then examined. Finally, for a particular RDE configuration, it is found that direct performance comparison can be made with a straight-tube pulse detonation engine (PDE). Results show that they ar...
Desire for a more efficient air breathing engine has shifted research attention to the Rotating Deto...
Two models are proposed for rotating detonation engine performance. The first model is motivated by...
Cette thèse s’inscrit dans le domaine de la simulation numérique appliquée à la propulsion. Le moteu...
A quasi-two-dimensional, computational fluid dynamic (CFD) simulation of a rotating detonation engin...
A rotating detonation engine (RDE) configuration whereby the working fluid enters and exits in a pre...
An instability is described which arises in computational fluid dynamic (CFD) simulations of semi-id...
A practical thermodynamic cycle model of a rotating detonation engine (RDE) is developed for the pur...
High-fidelity numerical simulations of an experimental rotating detonation engine with discrete fuel...
As turbine and rocket engine technology matures, performance increases between successive generation...
The potential higher performance of rotating detonation engines (RDEs), due to the constant volume c...
An analysis is presented of an experimental rig comprising a rotating detonation engine (RDE) with b...
A simplified, two-dimensional, computational fluid dynamic (CFD) simulation, with a reactive Euler s...
A series of 3- and 2-dimensional numerical simulations of a rotating detonation engine (RDE) are car...
To enhance the efficiency and capability of aeropropulsion platforms, step changes in thermal effici...
A cycle analysis model for an airbreathing, rotating detonation wave engine (RDE) is presented. The ...
Desire for a more efficient air breathing engine has shifted research attention to the Rotating Deto...
Two models are proposed for rotating detonation engine performance. The first model is motivated by...
Cette thèse s’inscrit dans le domaine de la simulation numérique appliquée à la propulsion. Le moteu...
A quasi-two-dimensional, computational fluid dynamic (CFD) simulation of a rotating detonation engin...
A rotating detonation engine (RDE) configuration whereby the working fluid enters and exits in a pre...
An instability is described which arises in computational fluid dynamic (CFD) simulations of semi-id...
A practical thermodynamic cycle model of a rotating detonation engine (RDE) is developed for the pur...
High-fidelity numerical simulations of an experimental rotating detonation engine with discrete fuel...
As turbine and rocket engine technology matures, performance increases between successive generation...
The potential higher performance of rotating detonation engines (RDEs), due to the constant volume c...
An analysis is presented of an experimental rig comprising a rotating detonation engine (RDE) with b...
A simplified, two-dimensional, computational fluid dynamic (CFD) simulation, with a reactive Euler s...
A series of 3- and 2-dimensional numerical simulations of a rotating detonation engine (RDE) are car...
To enhance the efficiency and capability of aeropropulsion platforms, step changes in thermal effici...
A cycle analysis model for an airbreathing, rotating detonation wave engine (RDE) is presented. The ...
Desire for a more efficient air breathing engine has shifted research attention to the Rotating Deto...
Two models are proposed for rotating detonation engine performance. The first model is motivated by...
Cette thèse s’inscrit dans le domaine de la simulation numérique appliquée à la propulsion. Le moteu...