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 …

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 …

[HTML][HTML] Criteria for hypersonic airbreathing propulsion and its experimental verification

Z Jiang, Z Zhang, LIU Yunfeng, W Chun… - Chinese Journal of …, 2021 - Elsevier
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 …

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 …

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 …

Experimental study of detonation limits in methane-oxygen mixtures: Determining tube scale and initial pressure effects

B Zhang, H Liu, B Yan, HD Ng - Fuel, 2020 - Elsevier
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 …

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 …

Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model

P Yang, H Teng, Z Jiang, HD Ng - Combustion and Flame, 2018 - Elsevier
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 …

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 …

Numerical study of wedge-induced oblique detonations in unsteady flow

P Yang, HD Ng, H Teng - Journal of Fluid Mechanics, 2019 - cambridge.org
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 …