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 …

Supersonic spray combustion subject to scramjets: Progress and challenges

Z Ren, B Wang, G Xiang, D Zhao, L Zheng - Progress in Aerospace …, 2019 - Elsevier
Supersonic spray combustion is one of the most significant physiochemical processes that
occurs in the scramjet propulsion system, and related research can motivate the …

The effect of carbon dioxide emissions on the building energy efficiency

J Min, G Yan, AM Abed, S Elattar, MA Khadimallah… - Fuel, 2022 - Elsevier
During this anthropocentric period, sustainable energy supply and climate changing could
be a main source of problem for human being. Scientists believe that the ratio of climate …

[HTML][HTML] Irregular heat source impact on Carreau nanofluid flowing via exponential expanding cylinder: A thermal case study

M Akram, W Jamshed, BS Goud, AA Pasha… - Case Studies in Thermal …, 2022 - Elsevier
In the Carreau nanofluid (CNF) flow, the transmission of heat through the stretching cylinder
is observed in two terms, one is non-linear stretching and other is irregular heat sink/source …

The influence of wall roughness on detonation limits in hydrogen–oxygen mixture

B Zhang - Combustion and Flame, 2016 - Elsevier
In this study, wall roughness is generated by inserting a Shchelkin spiral with different wire
diameter (δ) and pitch (L s). Roughness is defined as the ratio δ/L s. The effect of tube wall …

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 …

The effect of instability of detonation on the propagation modes near the limits in typical combustible mixtures

B Zhang, H Liu, Y Li - Fuel, 2019 - Elsevier
At the near-limit conditions, the behavior of detonation propagation manifests unstable
modes; those modes are classified into three types, ie, steady mode, fluctuation mode and …

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 …