Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture

Studies of spray combustion in engines or furnaces are complicated due to the multiplicity of dependent parameters. The flame propagation rate in the two-phase-environment must be analysed in isolation from the complex processes of fuel injection and mixing. Therefore, a fundamental study of droplet...

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Main Authors: Sulaiman, S. A., Abdul Karim, Z. A., Lawes, M.
Format: Conference or Workshop Item
Published: 2008
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Online Access:http://eprints.utp.edu.my/822/1/HFT_ID_0349.pdf
http://eprints.utp.edu.my/822/
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spelling my.utp.eprints.8222017-01-19T08:26:45Z Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture Sulaiman, S. A. Abdul Karim, Z. A. Lawes, M. TJ Mechanical engineering and machinery Studies of spray combustion in engines or furnaces are complicated due to the multiplicity of dependent parameters. The flame propagation rate in the two-phase-environment must be analysed in isolation from the complex processes of fuel injection and mixing. Therefore, a fundamental study of droplet cloud combustion is required to investigate the parameters of importance. In a study of turbulent flame combustion of droplet and vapour mixtures a spherical explosion vessel, fuel-air aerosols are generated by expansion of a gaseous mixture using the Wilson cloud chamber principle. With this technique suspended droplets would appear when the temperature of the mixture drops below the saturation value. The size of the droplets increases as the temperature is further reduced. A problem encountered in conducting this experiment is that the time for the onset of droplet formation with respect to the start of expansion is not known. Therefore, it would be difficult, with the absence of such information, to plan the pre-ignition condition of the droplet-vapour mixture. Moreover, in order to compare the experimental results with those from other researches, an estimation of the number of droplets within the explosion vessel is required. In this paper, the application of a laser attenuation technique to determine the onset of nucleation of liquid droplet suspensions within turbulent fuel-air aerosol is presented. The laser attenuation technique is supported by a Class-3A laser that is collimated by a set of optical lens. The amount of laser light that passes through the vessel reduces with the presence of droplets. The relationship between the number of droplets within the aerosol and the laser attenuation is described by the Beer-Lambert law. 2008 Conference or Workshop Item PeerReviewed application/pdf http://eprints.utp.edu.my/822/1/HFT_ID_0349.pdf Sulaiman, S. A. and Abdul Karim, Z. A. and Lawes, M. (2008) Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture. In: International Conference on Mechanical and Manufacturing Engineering, May 2008, Johor Bahru, Malaysia. http://eprints.utp.edu.my/822/
institution Universiti Teknologi Petronas
building UTP Resource Centre
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Petronas
content_source UTP Institutional Repository
url_provider http://eprints.utp.edu.my/
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Sulaiman, S. A.
Abdul Karim, Z. A.
Lawes, M.
Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture
description Studies of spray combustion in engines or furnaces are complicated due to the multiplicity of dependent parameters. The flame propagation rate in the two-phase-environment must be analysed in isolation from the complex processes of fuel injection and mixing. Therefore, a fundamental study of droplet cloud combustion is required to investigate the parameters of importance. In a study of turbulent flame combustion of droplet and vapour mixtures a spherical explosion vessel, fuel-air aerosols are generated by expansion of a gaseous mixture using the Wilson cloud chamber principle. With this technique suspended droplets would appear when the temperature of the mixture drops below the saturation value. The size of the droplets increases as the temperature is further reduced. A problem encountered in conducting this experiment is that the time for the onset of droplet formation with respect to the start of expansion is not known. Therefore, it would be difficult, with the absence of such information, to plan the pre-ignition condition of the droplet-vapour mixture. Moreover, in order to compare the experimental results with those from other researches, an estimation of the number of droplets within the explosion vessel is required. In this paper, the application of a laser attenuation technique to determine the onset of nucleation of liquid droplet suspensions within turbulent fuel-air aerosol is presented. The laser attenuation technique is supported by a Class-3A laser that is collimated by a set of optical lens. The amount of laser light that passes through the vessel reduces with the presence of droplets. The relationship between the number of droplets within the aerosol and the laser attenuation is described by the Beer-Lambert law.
format Conference or Workshop Item
author Sulaiman, S. A.
Abdul Karim, Z. A.
Lawes, M.
author_facet Sulaiman, S. A.
Abdul Karim, Z. A.
Lawes, M.
author_sort Sulaiman, S. A.
title Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture
title_short Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture
title_full Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture
title_fullStr Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture
title_full_unstemmed Laser Attenuation Technique for Measurements of Droplets in a Turbulent Fuel-Air Aerosol Mixture
title_sort laser attenuation technique for measurements of droplets in a turbulent fuel-air aerosol mixture
publishDate 2008
url http://eprints.utp.edu.my/822/1/HFT_ID_0349.pdf
http://eprints.utp.edu.my/822/
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score 13.209306