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contributor authorLanjekar, R. D.
contributor authorDeshmukh, D.
date accessioned2019-09-18T09:05:06Z
date available2019-09-18T09:05:06Z
date copyright3/18/2019 12:00:00 AM
date issued2019
identifier issn0742-4795
identifier othergtp_141_07_071020.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4258675
description abstractThe vapor mass fraction distribution of the multicomponent surrogate of diesel and biodiesel fuel is studied using multicomponent evaporation model at engine-relevant conditions. The numerical model is validated with experimental liquid tip penetration and vapor penetration for diesel and biodiesel. The vapor distribution for a multicomponent surrogate is significantly different than that of single-component fuel. The tetradecane, single-component surrogate for diesel has different vapor mass distribution unlike in multicomponent diesel fuel. The spatial mass fraction distribution profile of biodiesel is found to be the function of volatility differential of the pure components and their proportion in the composition. The vapor mass fraction distribution for biodiesel of palm and soybean is found to be similar to that of their single-component surrogate due to comparable volatility of components of these biodiesels. However, methyl laurate in coconut biodiesel has volatility differential with other components and also has a significant share of 40% to 50% in the coconut biodiesel composition. The change in percentage of methyl laurate in coconut composition is found to have strong impact on vapor distribution. The vapor mass fraction distribution is observed to be affected by the change in the biodiesel composition specifically volatile component.
publisherAmerican Society of Mechanical Engineers (ASME)
titleMulticomponent Evaporation Characteristics of Biodiesel Sprays
typeJournal Paper
journal volume141
journal issue7
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4043027
journal fristpage71020
journal lastpage071020-7
treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 007
contenttypeFulltext


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