Combustion Diagnostics

A special issue of Fire (ISSN 2571-6255). This special issue belongs to the section "Mathematical Modelling and Numerical Simulation of Combustion and Fire".

Deadline for manuscript submissions: 30 June 2024 | Viewed by 4132

Special Issue Editor


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Guest Editor
School of Aerospace Engineering, Xiamen University, Xiamen 361005, China
Interests: combustion diagnostics

Special Issue Information

Dear Colleagues,

Optical diagnostics has been identified as a useful tool for understanding the fundamental physics of turbulent combustion. Up until now, various diagnostic methods across the full range of the light spectrum have been extensively studied and demonstrated. Ultraviolet-C (UVC) spectral band refers to the spectrum of light between 200 and 280 nm. Solar radiation in this spectral interval does not reach the Earth’s surface due to ozone absorption. Therefore, this spectral domain is also called “solar blind”. Such solar-blindness provides a unique measurement opportunity, with low background noise and high SNR. This Special Issue is dedicated to the most recent advances in diagnostics utilizing the UVC band and its applications in combustion and propulsion systems.

Dr. Wenjiang Xu
Guest Editor

Manuscript Submission Information

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Published Papers (3 papers)

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Research

20 pages, 15937 KiB  
Article
Analysis of Flow Field Characteristics of the Propane Jet Combustion Flame
by Shengnan Li, Jingjing Guo, Zheng Chi, Bo Zhao and Shuai Zhao
Fire 2023, 6(12), 464; https://doi.org/10.3390/fire6120464 - 07 Dec 2023
Viewed by 1241
Abstract
In order to effectively prevent fire accidents and improve fire management capability, this paper describes the independent designs and builds of an experimental low-cost particle image velocimetry platform for a propane jet combustion flame using traditional mutual correlation theory. The particle image velocimetry [...] Read more.
In order to effectively prevent fire accidents and improve fire management capability, this paper describes the independent designs and builds of an experimental low-cost particle image velocimetry platform for a propane jet combustion flame using traditional mutual correlation theory. The particle image velocimetry (PIV) algorithm is written based on MATLAB software, allowing it to realise image preprocessing, multi-level grid window deformation inter-correlation calculations, and other functions. Fluid flow velocity and vorticity are used as entry points to study the flame combustion mechanism. The air flow field and vorticity above the propane jet flame are analysed. The results show that, from the level of fluid flow velocity, the maximum fluid flow velocity in the test area does not exceed 0.23 m/s, and the maximum transverse fluid flow velocity is close to 0.15 m/s. Additionally, the longitudinal fluid flow velocity is opposite the upper and lower portions of the longitudinal flow velocity, and there is a swirling phenomenon in the propane flame jet. From the vorticity level, the closer to the centre of the jet in the vortex plane, the faster the air flow speed, and simultaneously, in the upper and lower parts of the vortex, the air flow travels in the opposite direction and is of equal size. The particle image velocimetry platform that was independently designed in this study can efficiently characterise the dynamic flow field and the flow characteristics of complex combustion chambers, simultaneously ensuring high efficiency and reducing research costs. It provides a measurement method and experimental basis for the development of fire extinguishing equipment and numerical simulation, while also helping us to carry out a series of subsequent studies on fire extinguishing mechanisms. Full article
(This article belongs to the Special Issue Combustion Diagnostics)
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12 pages, 3233 KiB  
Article
New Insight into the Effects of Gaseous CO2 on Spherically Symmetric Droplet Flames
by Ter-Ki Hong and Seul-Hyun Park
Fire 2023, 6(12), 461; https://doi.org/10.3390/fire6120461 - 04 Dec 2023
Viewed by 1253
Abstract
This study investigated the effect of CO2 on the burning behavior and radiative properties of a single ethanol droplet flame in microgravity. Measurements of the droplet burning rate, the flame size and temperature, and the radiative emissions were performed, under microgravity conditions [...] Read more.
This study investigated the effect of CO2 on the burning behavior and radiative properties of a single ethanol droplet flame in microgravity. Measurements of the droplet burning rate, the flame size and temperature, and the radiative emissions were performed, under microgravity conditions for ethanol droplets burning in N2 and CO2 environments, using the 1.5 s drop tower facilities at the Korea Maritime and Ocean University (KMOU). The non-monotonic sooting behaviors (caused by the elevated O2 concentrations) were found to have a significant influence on radiative heat losses in N2 environments, resulting in non-linear droplet burning behaviors with O2 concentrations. Due to the unique nature of CO2 in microgravity, which absorbs radiative energy from the flame and raises the temperatures of the surrounding gases, the CO2 environments suppressed the radiative heat losses from the flame, regardless of the non-monotonic sooting behavior observed at the higher O2 concentrations. These experimental findings highlight the complicated physics of CO2 gas radiation in microgravity, which has not been quantitatively explored. Full article
(This article belongs to the Special Issue Combustion Diagnostics)
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17 pages, 3838 KiB  
Article
Fire Ignition and Propagation in Hidden Zones of Aircrafts: A Novel Confined Fire Apparatus (CFA) for Flame Spreading Investigation
by Vasiliki N. Papadogianni, Alexandros Romeos, Athanasios Giannadakis, Konstantinos Perrakis and Thrassos Panidis
Fire 2023, 6(8), 292; https://doi.org/10.3390/fire6080292 - 31 Jul 2023
Viewed by 954
Abstract
This research investigated potential fire hazards originating in hidden areas of pressurized sections of aircrafts. The objective was to establish a laboratory-scale flammability test method to predict the behavior of fire propagation under real fire conditions. A confined fire apparatus (CFA) was designed [...] Read more.
This research investigated potential fire hazards originating in hidden areas of pressurized sections of aircrafts. The objective was to establish a laboratory-scale flammability test method to predict the behavior of fire propagation under real fire conditions. A confined fire apparatus (CFA) was designed and constructed, and several tests were conducted to better understand the involved mechanisms and their consequences and to estimate flame spreading in hidden-zone fires. The experimental facility and flame-spreading results obtained for a typical material involved in hidden fires, specifically a ceiling panel, were presented and discussed. The experimental facility consisted of a narrow passage where a fire was initiated using a burner on a specimen exposed to a controlled heat flux. Experiments were conducted in the absence of forced airflow. Flame spreading was estimated through visual monitoring of fire development or temperature measurements at specific locations in the specimen. Both methods yielded similar results. The flame spread velocity in relation to the imposed heat flux allowed for the estimation of the critical heat flux for spreading q˙sp,cr and for ignition q˙ig,cr; the corresponding temperatures, Ts,min and Tig; and the flame spread parameter Φ. Full article
(This article belongs to the Special Issue Combustion Diagnostics)
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