Enhancing detonation propulsion with jet in cross-flow: A comprehensive review
B Zhang - Progress in Aerospace Sciences, 2024 - Elsevier
Compared with traditional deflagration-based systems, detonation-based propulsion
systems offer significant potential benefits in terms of efficiency and specific impulses in the …
systems offer significant potential benefits in terms of efficiency and specific impulses in the …
Standing oblique detonation for hypersonic propulsion: A review
Z Jiang - Progress in Aerospace Sciences, 2023 - Elsevier
Standing oblique detonation is a unique pressure-gain combustion phenomenon for
hypersonic ramjet propulsion, and its research has been related with supersonic combustion …
hypersonic ramjet propulsion, and its research has been related with supersonic combustion …
[HTML][HTML] Criteria for hypersonic airbreathing propulsion and its experimental verification
Hypersonic airbreathing propulsion is one of the top techniques for future aerospace flight,
but there are still no practical engines after seventy years' development. Two critical issues …
but there are still no practical engines after seventy years' development. Two critical issues …
Ignition behavior and the onset of quasi-detonation in methane-oxygen using different end wall reflectors
B Zhang, Y Li, H Liu - Aerospace Science and Technology, 2021 - Elsevier
The shock wave focusing technique is beneficial to the development of detonation-based
engines, which can shorten the long run-up distance that is usually required for a …
engines, which can shorten the long run-up distance that is usually required for a …
Numerical study on transition structures of oblique detonations with expansion wave from finite-length cowl
GX Xiang, X Gao, WJ Tang, XZ Jie, X Huang - Physics of Fluids, 2020 - pubs.aip.org
The oblique detonation wave (ODW) triggered by a semi-infinite cowl or wedge has been
widely studied, but the effects of finite-length cowls require further clarification to enhance …
widely studied, but the effects of finite-length cowls require further clarification to enhance …
Experimental study of detonation limits in methane-oxygen mixtures: Determining tube scale and initial pressure effects
In this paper, detonation limits in stoichiometric methane-oxygen mixtures with varying tube
inner diameter and initial mixture pressure were investigated. Detonations in tubes with …
inner diameter and initial mixture pressure were investigated. Detonations in tubes with …
Oblique detonation waves induced by two symmetrical wedges in hydrogen-air mixtures
G Xiang, Y Zhang, X Gao, H Li, X Huang - Fuel, 2021 - Elsevier
An understanding of oblique detonation waves (ODWs) has inherent research value for high-
speed compressible reacting flow and hypersonic propulsion. In this paper, the interactions …
speed compressible reacting flow and hypersonic propulsion. In this paper, the interactions …
Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model
Oblique detonations induced by two-dimensional, semi-infinite wedges are simulated by
solving numerically the reactive Euler equations with a two-step induction-reaction kinetic …
solving numerically the reactive Euler equations with a two-step induction-reaction kinetic …
Morphology of oblique detonation waves in a stoichiometric hydrogen–air mixture
H Teng, C Tian, Y Zhang, L Zhou… - Journal of Fluid …, 2021 - cambridge.org
Although the morphology of oblique detonation waves (ODWs) has been widely studied, it
remains impossible to predict the wave systems in the initiation region, which is a critical …
remains impossible to predict the wave systems in the initiation region, which is a critical …
Numerical study of wedge-induced oblique detonations in unsteady flow
Oblique detonation waves (ODWs) have been studied widely to facilitate their employment
in hypersonic propulsion, but the effects of continuous unsteady inflow have never been …
in hypersonic propulsion, but the effects of continuous unsteady inflow have never been …