Results 71 to 80 of about 3,707 (264)

Study of combustion flow field in a scramjet engine under inflow oscillation variations based on OpenFOAM

open access: yesCase Studies in Thermal Engineering
In this study, a compressible supersonic numerical model was established based on the open-source computational fluid dynamics software OpenFOAM. The supersonic air inflow was set in sinusoidal variation and gas hydrogen was employed as fuel for the DLR ...
Changhao Wang   +6 more
doaj   +1 more source

Pulsed combustion of hydrocarbon fuels in a supersonic model combustor [PDF]

open access: yes, 2011
Pulsed combustion of hydrocarbon fuels (ethylene and kerosene) in a Mach number 2.5 supersonic model combustor was experimentally investigated using a pulse spark igniter located in the center of a cavity.
Li JG(李建国)   +5 more
core  

Durable Fuel Cell Cathode Enabled by Pt Embedded Nanoscale Carbon Network via a Scalable Process

open access: yesCarbon Energy, EarlyView.
Platinum nanoparticles embedded nanoscale carbon network (Pt‐e‐Cn) are developed via a scalable flame spray pyrolysis process. Proton exchange membrane fuel cells (PEMFC) employing mesoporous Pt‐e‐Cn cathode electrocatalysts exhibit exceptional durability without compromising performance.
Suriya Venkatesan   +10 more
wiley   +1 more source

Research on Effect of Pollution Gas Components Based on Computational Simulation and Computational Fluid Dynamics Technology on Supersonic Combustion

open access: yesChemical Engineering Transactions, 2017
Based on computational simulation and computational fluid dynamics (CFD), this paper analyzes and compares the effects of incoming flow with clean air and air containing CO2/H2O pollution components on the performance of supersonic combustion of hydrogen
Xi Wang
doaj   +1 more source

Green and sustainable synthesis of magnetite from copper slag via citrate complexation for methylene blue dye removal from water

open access: yesThe Canadian Journal of Chemical Engineering, EarlyView.
Abstract This study proposes a novel, green, and sustainable method for synthesizing magnetic iron oxides from metallurgical copper slag (CS), leveraging its iron content as a valuable resource. Iron was extracted via acid leaching using edible citric acid (ECA), forming a citrate–iron complex (CSL), which was subsequently thermally decomposed at 300°C
Melisa Portilla‐Sangabriel   +4 more
wiley   +1 more source

Chemical timescale analysis of the Partially Stirred Reactor model for a hydrogen-fuelled scramjet

open access: yesResults in Engineering
Scramjet engines offer a promising option for powering hypersonic vehicles, although the unique characteristics of supersonic combustion present numerous challenges.
Alessandro Piscopo   +3 more
doaj   +1 more source

Photothermal bubble: Dynamics, manipulation, and applications

open access: yesDroplet, EarlyView.
As a versatile platform for bubble manipulation, photothermal techniques empower diverse operations: planar translation by scanning the laser spot, sustained periodic bouncing from competing thermal and hydrodynamic flows, and even guided 3D trajectories achieved by tailoring the heating configuration.
Man Hu, Feng Wang, Daosheng Deng
wiley   +1 more source

Characteristic scales in supersonic combustion

open access: yes, 2013
The characteristic length scales in supersonic combustion and the related influence factors were calculated and analyzed. In addition, using the hydrogen, ethylene and kerosene as fuels, the operating range of scramjet under the practical flight ...
Li XP(李晓鹏)   +2 more
core  

Experimental Investigation of Microwave-Assisted Kerosene Supersonic Combustion

open access: yes
The microwave-assisted kerosene combustion in supersonic flow was invested experimentally using a novel microwave-flame coupling method. The experiment used a direct-connected system, with a horn antenna employed to introduce microwaves into the ...
Ren, Yaohui   +3 more
core   +2 more sources

Combustion of Vaporized Kerosene in Supersonic Model Combustors with Dislocated Dual Cavities

open access: yes, 2014
Supersonic combustion of vaporized kerosene in a Mach 2.5 model combustor with a total temperature of 1500 K and a total pressure of 1.3 MPa was experimentally investigated for an optimal integration of the cavity-based flameholder and the fuel injection
王晶   +4 more
core   +1 more source

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