Javascript must be enabled to continue!
Study on Initiation Characteristics of Oblique Detonation Induced by Hydrogen Jets in Acetylene-Air Mixtures
View through CrossRef
In this paper, effects of hydrogen jets on the initiation characteristics of oblique detonation wave (ODW) are investigated, the two-dimensional (2D) multi-component NS equations considering chemical reactions are solved. Influences of the transverse jet on flow field characteristics of the ODW are studied, including the initiation characteristics, the wave structures, and the state parameters. The existence of the jet changes the ignited mode of the ODW from double Mach interaction to single Mach interaction. Several wave configurations and their transitions induced by the jets are observed, including the classic deflagration-to-ODW transition, jet-induced oblique shock wave (OSW) in front of the transverse jet and rapidly develops into ODW, and ODW that generated directly in front of the transverse jet. Two types of relationships are obtained between the detonation distance and the position of the transverse jet: the U-shaped curve at low flow discharge and the positive correlation at high flow discharge. Furthermore, the viscous effect has significant influence on the flow field characteristics of ODW, it promotes the transition between these initiation modes and shortens the initiation distance of oblique detonation.
Title: Study on Initiation Characteristics of Oblique Detonation Induced by Hydrogen Jets in Acetylene-Air Mixtures
Description:
In this paper, effects of hydrogen jets on the initiation characteristics of oblique detonation wave (ODW) are investigated, the two-dimensional (2D) multi-component NS equations considering chemical reactions are solved.
Influences of the transverse jet on flow field characteristics of the ODW are studied, including the initiation characteristics, the wave structures, and the state parameters.
The existence of the jet changes the ignited mode of the ODW from double Mach interaction to single Mach interaction.
Several wave configurations and their transitions induced by the jets are observed, including the classic deflagration-to-ODW transition, jet-induced oblique shock wave (OSW) in front of the transverse jet and rapidly develops into ODW, and ODW that generated directly in front of the transverse jet.
Two types of relationships are obtained between the detonation distance and the position of the transverse jet: the U-shaped curve at low flow discharge and the positive correlation at high flow discharge.
Furthermore, the viscous effect has significant influence on the flow field characteristics of ODW, it promotes the transition between these initiation modes and shortens the initiation distance of oblique detonation.
Related Results
Advances on Deflagration to Detonation Transition Methods in Pulse Detonation Engines
Advances on Deflagration to Detonation Transition Methods in Pulse Detonation Engines
Pulse detonation engines (PDEs) have become a transformative technology in the field of aerospace propulsion due to the high thermal efficiency of detonation combustion. However, i...
Detonation wave propagation in micro-scale groove charges
Detonation wave propagation in micro-scale groove charges
The detonation wave propagation characteristics in micro-scale groove charges are very important for optimizing the structure of the Micro-Electro-Mechanics System explosive train ...
Combustion Characteristics in Rotating Detonation Engines
Combustion Characteristics in Rotating Detonation Engines
A lot of studies on rotating detonation engines have been carried out due to the higher thermal efficiency. However, the number, rotating directions, and intensities of rotating de...
Recirculation effects on detonation in a flow-through ramjet combustor
Recirculation effects on detonation in a flow-through ramjet combustor
The application of detonation combustion to enhance the combustion performance of ramjets requires careful consideration of combustion stability. Recirculation zones are critical f...
Experimental Consideration of the Detonation Expansion Wave Limit
Experimental Consideration of the Detonation Expansion Wave Limit
The pressure time-history associated with a propagating detonation within a pipe can be reasonably well described using a one-dimensional model. These models describe the advanceme...
Couplage accrétion-éjection dans les microquasars et sources X ultralumineuses
Couplage accrétion-éjection dans les microquasars et sources X ultralumineuses
Dans l'Univers, des processus d'éjection de matière sont observés dans un large éventail de systèmes accrétants ; néanmoins, la formation et la propagation de ces jets sont encore ...
Investigation on the Blade Leading-Edge Film Cooling With Normal and Staggered-Oblique Impinging Jets
Investigation on the Blade Leading-Edge Film Cooling With Normal and Staggered-Oblique Impinging Jets
Abstract
Film cooling is widely employed to protect the external wall of the turbine blade leading edge from hot gas exposure, while impingement cooling is a comm...
Multiphase Rotating Detonation Engine
Multiphase Rotating Detonation Engine
Abstract
The first experimental evidence of a solid-gas multiphase rotating detonation engine. Coal particles, carbon black with a volatility of 1% and a carbon conc...

