The Rotating Detonation Engine (RDE) has gained increasing attention in recent years for its potential advantages over typical deflagration combustion. A Micro-RDE design with an outer diameter of 28mm operating on Nitrous Oxide and Ethylene was recently developed, which stretched the limits of small-scale detonation engines. The testing on this rig has shown a stable one wave mode detonation with frequencies reaching 16.8 kHz. Key parameters that influence the detonation wave mode are cell size, fill height, and wave speed, which are heavily influence d by injection schemes. Previous testing utilized a partially premixed jets in crossflow (JIC) injection scheme, while tests before that used a traditional JIC scheme. A Simplex and Counter-j...
The potential higher performance of rotating detonation engines (RDEs), due to the constant volume c...
A modular laboratory rotating detonation engine (RDE) for combined mass flowrates below 10 g/s has b...
A study is presented on the relationship between a pre-detonator and a detonation channel of an RDE....
The Rotating Detonation Engine (RDE) has been researched extensively in recent years, but the minimu...
A small scale RDE was designed with a channel diameter of 28 mm and channel gap of 2 mm and operated...
In light of the growing demand for more efficient aviation engines, detonation-based engines are bei...
Desire for a more efficient air breathing engine has shifted research attention to the Rotating Deto...
As the injection total pressure increases, the flow field in the combustion chamber of rotating deto...
Rotating detonation engines (RDEs) present great potential for significant improvement in efficiency...
Conventional engines are limited by the efficiency of their combustion mode. Compared to present con...
This work examines the mechanisms of reactant mixing in a model Rotating Detonation Engine (RDE) geo...
Detonation is a promising combustion mode to improve engine performance, increase combustion efficie...
Thesis (Master's)--University of Washington, 2019Radial propellant injection in the annular combusti...
The maturation of Brayton-cycle engines has led to a plateau in combustor performance where improvem...
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...
A modular laboratory rotating detonation engine (RDE) for combined mass flowrates below 10 g/s has b...
A study is presented on the relationship between a pre-detonator and a detonation channel of an RDE....
The Rotating Detonation Engine (RDE) has been researched extensively in recent years, but the minimu...
A small scale RDE was designed with a channel diameter of 28 mm and channel gap of 2 mm and operated...
In light of the growing demand for more efficient aviation engines, detonation-based engines are bei...
Desire for a more efficient air breathing engine has shifted research attention to the Rotating Deto...
As the injection total pressure increases, the flow field in the combustion chamber of rotating deto...
Rotating detonation engines (RDEs) present great potential for significant improvement in efficiency...
Conventional engines are limited by the efficiency of their combustion mode. Compared to present con...
This work examines the mechanisms of reactant mixing in a model Rotating Detonation Engine (RDE) geo...
Detonation is a promising combustion mode to improve engine performance, increase combustion efficie...
Thesis (Master's)--University of Washington, 2019Radial propellant injection in the annular combusti...
The maturation of Brayton-cycle engines has led to a plateau in combustor performance where improvem...
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...
A modular laboratory rotating detonation engine (RDE) for combined mass flowrates below 10 g/s has b...
A study is presented on the relationship between a pre-detonator and a detonation channel of an RDE....