Results 31 to 40 of about 419 (166)

Investigation on C2H4-Air combustion mode in a non-premixed rotating detonation combustor

open access: yesPropulsion and Power Research, 2022
Based on the working characteristics of the rotating detonation combustor, the combustion mode of C2H4-Air under non-premixed injection conditions is experimentally studied in this paper.
Shengbing Zhou   +4 more
doaj   +1 more source

Experimental Investigation of a Cylindrical Air-Breathing Continuous Rotating Detonation Engine with Different Nozzle Throat Diameters

open access: yesAerospace, 2022
A continuous detonation engine with various exhaust nozzles, analogous to typical scramjet cavity combustors with variable rear-wall heights, was adopted to perform a succession of cylindrical air-breathing continuous rotating detonation experiments ...
Guangyu Wang   +3 more
doaj   +1 more source

Influence of Gaseous Hydrogen Addition on Initiation of Rotating Detonation in Liquid Fuel–Air Mixtures

open access: yesEnergies, 2020
Hydrogen is the most common molecule in the universe. It is an excellent fuel for thermal engines: piston, turbojet, rocket, and, going forward, in thermonuclear power plants. Hydrogen is currently used across a range of industrial applications including
Jan Kindracki   +4 more
doaj   +1 more source

Numerical and boundary condition effects on the prediction of detonation engine behavior using detailed numerical simulations

open access: yesFrontiers in Aerospace Engineering, 2023
High-fidelity numerical simulations of an experimental rotating detonation engine with discrete fuel/air injection were conducted. A series of configurations with different feed-plenum pressures but with constant equivalence ratio were studied.
Takuma Sato   +2 more
doaj   +1 more source

Numerical Investigation on the Height of Detonation Wave in Rotating Detonation Engine

open access: yesJournal of Physics: Conference Series, 2022
Abstract Three-dimensional numerical simulations were conducted on a non-premixed rotating detonation engine (RDE) with different exhaust nozzles (i.e. without a nozzle, with a divergent nozzle, with a convergent nozzle, and with a Laval nozzle).
Sainan Xue   +6 more
openaire   +1 more source

Experimental Study on the Propagation Characteristics of Rotating Detonation Wave with Rich Combustion Gas in Solid Ram Engine [PDF]

open access: yesHangkong bingqi
In order to study the rotational detonation characteristics of rich combustion gas in solid ramjet engines, this paper replaces solid rich combustion gas with CH4/CO/H2 mixture as fuel and uses ambient temperature air as oxidant to investigate the ...
Weng Chunsheng, Han Jiaxiang, Bai Qiaodong, Liu Zhuyong, Zheng Quan
doaj   +1 more source

Visualization of the Detonation Wave Structure in a Small-Scale Hydrogen–Oxygen Rotating Detonation Combustor

open access: yesAerospace
This study presents the high-speed visualization of the detonation wave structure in a small-scale hydrogen–oxygen rotating detonation combustor. A 68 mm Rotating Detonation Combustor was modified with a quartz-glass ring, such that radial optical access
Wolfgang Armbruster   +7 more
doaj   +1 more source

Rotating Detonation Combustion for Advanced Liquid Propellant Space Engines

open access: yesAerospace, 2022
Rotating (also termed continuous spin) detonation technology is gaining interest in the global research and development community due to the potential for increased performance.
Stephen D. Heister   +5 more
doaj   +1 more source

Experimental study on effects of nozzles and combustors on the rotating detonation rocket engine in pulse operation

open access: yesResults in Engineering
The rotating detonation engine (RDE) is an innovative pressure-gain combustion device that harnesses detonation waves for efficient fuel combustion.
Guining Liu   +6 more
doaj   +1 more source

Operation regimes in a rotating detonation combustor [PDF]

open access: yesINCAS Bulletin
This paper presents an exploration of the operational envelope of a Rotating Detonation Combustor based on the design of the research group at the University of Southampton.
George Ionut VRABIE   +5 more
doaj   +1 more source

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